def setup(self):
# create the DVGeo object that does the computations
if self.options["ffd_file"] is not None:
# we are doing an FFD-based DVGeo
ffd_file = self.options["ffd_file"]
self.DVGeo = DVGeometry(ffd_file)
if self.options["vsp_file"] is not None:
# we are doing a VSP based DVGeo
vsp_file = self.options["vsp_file"]
vsp_options = self.options["vsp_options"]
self.DVGeo = DVGeometryVSP(vsp_file, comm=self.comm, **vsp_options)
self.DVCon = DVConstraints()
self.DVCon.setDVGeo(self.DVGeo)
self.omPtSetList = []
def test_spanwise_dvs(self, train=False, refDeriv=False):
"""
Test spanwise_dvs
"""
# refFile = os.path.join(self.base_path,'ref/test_DVGeometry_spanwise_dvs.ref')
# with BaseRegTest(refFile, train=train) as handler:
# handler.root_print("Test spanwise local variables writing function")
meshfile = os.path.join(self.base_path, "../../input_files/c172.stl")
ffdfile = os.path.join(self.base_path, "../../input_files/c172.xyz")
testmesh = mesh.Mesh.from_file(meshfile)
# test mesh dim 0 is triangle index
# dim 1 is each vertex of the triangle
# dim 2 is x, y, z dimension
# create a DVGeo object with a few local thickness variables
DVGeo = DVGeometry(ffdfile)
DVGeo.addSpanwiseLocalDV("shape", "i", lower=-0.5, upper=0.5, axis="y", scale=1.0)
# create a DVConstraints object for the wing
DVCon = DVConstraints()
DVCon.setDVGeo(DVGeo)
p0 = testmesh.vectors[:, 0, :] / 1000
v1 = testmesh.vectors[:, 1, :] / 1000 - p0
v2 = testmesh.vectors[:, 2, :] / 1000 - p0
DVCon.setSurface([p0, v1, v2])
leList = [[0.7, 0.0, 0.1], [0.7, 0.0, 2.4]]
teList = [[0.9, 0.0, 0.1], [0.9, 0.0, 2.4]]
nSpan = 10
nChord = 10
name = "thickness_con"
DVCon.addThicknessConstraints2D(leList, teList, nSpan, nChord, name=name)
size = DVGeo._getNDVSpanwiseLocal()
np.random.seed(0)
DVGeo.setDesignVars({"shape": (np.random.rand(size) - 0.5)})
funcs = {}
DVCon.evalFunctions(funcs)
# print(funcs)
for i in range(nChord):
for j in range(nSpan - 1):
np.testing.assert_allclose(funcs[name][i * nChord + j + 1], funcs[name][i * nChord + j], rtol=2e-15)
def generate_dvgeo_dvcon_c172(self):
meshfile = os.path.join(self.base_path, '../inputFiles/c172.stl')
ffdfile = os.path.join(self.base_path, '../inputFiles/c172.xyz')
testmesh = mesh.Mesh.from_file(meshfile)
# test mesh dim 0 is triangle index
# dim 1 is each vertex of the triangle
# dim 2 is x, y, z dimension
# create a DVGeo object with a few local thickness variables
DVGeo = DVGeometry(ffdfile)
nRefAxPts = DVGeo.addRefAxis("wing", xFraction=0.25, alignIndex="k")
self.nTwist = nRefAxPts - 1
def twist(val, geo):
for i in range(1, nRefAxPts):
geo.rot_z["wing"].coef[i] = val[i - 1]
DVGeo.addGeoDVGlobal(dvName="twist", value=[0] * self.nTwist, func=twist, lower=-10, upper=10, scale=1)
DVGeo.addGeoDVLocal("local", lower=-0.5, upper=0.5, axis="y", scale=1)
# create a DVConstraints object for the wing
DVCon =DVConstraints()
DVCon.setDVGeo(DVGeo)
p0 = testmesh.vectors[:,0,:] / 1000
v1 = testmesh.vectors[:,1,:] / 1000 - p0
v2 = testmesh.vectors[:,2,:] / 1000 - p0
DVCon.setSurface([p0, v1, v2])
return DVGeo, DVCon
def test_13b(self, train=False, refDeriv=False):
refFile = os.path.join(self.base_path,'ref/test_DVConstraints_13b.ref')
with BaseRegTest(refFile, train=train) as handler:
handler.root_print("Test 13: PlanarityConstraint, rectangular box")
ffdfile = os.path.join(self.base_path, '../inputFiles/2x1x8_rectangle.xyz')
DVGeo = DVGeometry(ffdfile)
DVGeo.addGeoDVLocal("local", lower=-0.5, upper=0.5, axis="y", scale=1)
# create a DVConstraints object with a simple plane consisting of 2 triangles
DVCon =DVConstraints()
DVCon.setDVGeo(DVGeo)
p0 = np.zeros(shape=(2,3))
p1 = np.zeros(shape=(2,3))
p2 = np.zeros(shape=(2,3))
vertex1 = np.array([0.5, -0.25, 0.0])
vertex2 = np.array([0.5, -0.25, 4.0])
vertex3 = np.array([-0.5, -0.25, 0.0])
vertex4 = np.array([-0.5, -0.25, 4.0])
p0[:,:] = vertex1
p2[:,:] = vertex4
p1[0,:] = vertex2
p1[1,:] = vertex3
v1 = p1 - p0
v2 = p2 - p0
DVCon.setSurface([p0, v1, v2])
DVCon.addPlanarityConstraint(origin=[0.,-0.25,2.0], planeAxis=[0.,1.,0.])
funcs, funcsSens = self.generic_test_base(DVGeo, DVCon, handler, checkDerivs=False)
# this should be coplanar and the planarity constraint shoudl be zero
handler.assert_allclose(funcs['DVCon1_planarity_constraints_0'], np.zeros(1),
name='planarity', rtol=1e-7, atol=1e-7)
DVGeo = DVGeometry(FFDFile) # DVGeo = DVGeometry_FFD(FFDFile)
DVGeo.addGeoDVLocal("shape", lower=-0.05, upper=0.05, axis="y", scale=1.0)
span = 1.0
pos = np.array([0.5]) * span
CFDSolver.addSlices("z", pos, sliceType="absolute")
# Add DVGeo object to CFD solver
CFDSolver.setDVGeo(DVGeo)
# rst dvgeo (end)
# ======================================================================
# DVConstraint Setup
# ======================================================================
# rst dvcon (beg)
DVCon = DVConstraints() # DVCon = DVConstraints_FFD_data()
DVCon.setDVGeo(DVGeo)
# Only ADflow has the getTriangulatedSurface Function
DVCon.setSurface(CFDSolver.getTriangulatedMeshSurface())
# Le/Te constraints
lIndex = DVGeo.getLocalIndex(0)
indSetA = []
indSetB = []
# print('lIndex.shape[0]',lIndex.shape[0])
for k in range(0, 1):
indSetA.append(lIndex[0, 0, k]) # all DV for upper and lower should be same but different sign
indSetB.append(lIndex[0, 1, k])
for k in range(0, 1):
indSetA.append(lIndex[-1, 0, k])
def createFittedWingFFD(surf, surfFormat, outFile, leList, teList, nSpan,
nChord, absMargins, relMargins, liftIndex):
"""
Generates a wing FFD with chordwise points that follow the airfoil geometry.
Parameters
----------
surf : pyGeo object or list or str
The surface around which the FFD will be created.
See the documentation for :meth:`pygeo.DVConstraints.setSurface` for details.
surfFormat : str
The surface format.
See the documentation for :meth:`pygeo.DVConstraints.setSurface` for details.
outFile : str
Name of output file written in PLOT3D format.
leList : list or array
List or array of points (of size Nx3 where N is at least 2) defining the 'leading edge'.
teList : list or array
Same as leList but for the trailing edge.
nSpan : int or list of int
Number of spanwise sections in the FFD.
Use a list of length N-1 to specify the number for each segment defined by leList and teList
and to precisely match intermediate locations.
nChord : int
Number of chordwise points in the FFD.
absMargins : list of float
List with 3 items specifying the absolute margins in the [chordwise, spanwise, thickness] directions.
This is useful for areas where the relative margin is too small, such as the trailing edge or wing tip.
The total margin is the sum of the absolute and relative margins.
relMargins : list of float
List with 3 items specifying the relative margins in the [chordwise, spanwise, thickness] directions.
Relative margins are applied as a fraction of local chord, wing span, and local thickness.
The total margin is the sum of the absolute and relative margins.
liftIndex : int
Index specifying which direction lift is in (same as the ADflow option).
Either 2 for the y-axis or 3 for the z-axis.
This is used to determine the wing's spanwise direction.
Examples
--------
>>> CFDSolver = ADFLOW(options=aeroOptions)
>>> surf = CFDSolver.getTriangulatedMeshSurface()
>>> surfFormat = "point-vector"
>>> outFile = "wing_ffd.xyz"
>>> nSpan = [4, 4]
>>> nChord = 8
>>> relMargins = [0.01, 0.001, 0.01]
>>> absMargins = [0.05, 0.001, 0.05]
>>> liftIndex = 3
>>> createFittedWingFFD(surf, surfFormat, outFile, leList, teList, nSpan, nChord, absMargins, relMargins, liftIndex)
"""
# Import inside this function to avoid circular imports
from pygeo import DVConstraints
# Set the triangulated surface in DVCon
DVCon = DVConstraints()
DVCon.setSurface(surf, surfFormat=surfFormat)
# Get the surface intersections; surfCoords has dimensions [nSpanTotal, nChord, 2, 3]
surfCoords = DVCon._generateIntersections(leList,
teList,
nSpan,
nChord,
surfaceName="default")
nSpanTotal = np.sum(nSpan)
# Initialize FFD coordinates to the surface coordinates
FFDCoords = surfCoords.copy()
# Swap axes to get the FFD coordinates into PLOT3D ordering [x, y, z, 3]
FFDCoords = np.swapaxes(FFDCoords, 0, 1) # [nChord, nSpanTotal, 2, 3]
if liftIndex == 2:
# Swap axes again so that z is the spanwise direction instead of y
FFDCoords = np.swapaxes(FFDCoords, 1, 2) # [nChord, 2, nSpanTotal, 3]
# Assign coordinates and dimensions in each direction
# x is always the chordwise direction
leadingEdge = FFDCoords[0, :, :, 0]
trailingEdge = FFDCoords[-1, :, :, 0]
Nx = nChord
# y and z depend on the liftIndex
if liftIndex == 2:
root = FFDCoords[:, :, 0, 2]
tip = FFDCoords[:, :, -1, 2]
upperSurface = FFDCoords[:, 0, :, 1]
lowerSurface = FFDCoords[:, 1, :, 1]
Ny = 2
Nz = nSpanTotal
elif liftIndex == 3:
root = FFDCoords[:, 0, :, 1]
tip = FFDCoords[:, -1, :, 1]
upperSurface = FFDCoords[:, :, 1, 2]
lowerSurface = FFDCoords[:, :, 0, 2]
Ny = nSpanTotal
Nz = 2
else:
raise ValueError("liftIndex must be 2 (for y-axis) or 3 (for z-axis)")
# Add margins to FFD coordinates
chordLength = trailingEdge - leadingEdge
leadingEdge -= chordLength * relMargins[0] + absMargins[0]
trailingEdge += chordLength * relMargins[0] + absMargins[0]
span = np.max(tip - root)
root -= span * relMargins[1] + absMargins[1]
tip += span * relMargins[1] + absMargins[1]
thickness = upperSurface - lowerSurface
upperSurface += thickness * relMargins[2] + absMargins[2]
lowerSurface -= thickness * relMargins[2] + absMargins[2]
# Write FFD file
f = open(outFile, "w")
f.write("1\n")
f.write(f"{Nx} {Ny} {Nz}\n")
for ell in range(3):
for k in range(Nz):
for j in range(Ny):
for i in range(Nx):
f.write("%.15f " % (FFDCoords[i, j, k, ell]))
f.write("\n")
f.close()
def test_spanwise_dvs(self, train=False, refDeriv=False):
refFile = os.path.join(self.base_path, "ref/test_Cylinder_spanwise_dvs.ref")
with BaseRegTest(refFile, train=train) as handler:
handler.root_print("Test 1: Basic FFD, global DVs")
radius = 1.0
height = 10.0
DVCon = DVConstraints()
surf = self.make_cylinder_mesh(radius, height)
DVCon.setSurface(surf)
# DVCon.writeSurfaceTecplot('cylinder_surface.dat')
ffd_name = os.path.join(self.base_path, "../../input_files/cylinder_ffd.xyz")
self.make_ffd(ffd_name, radius, height)
DVGeo = DVGeometry(ffd_name)
DVGeo.addSpanwiseLocalDV("shape", "i", lower=-0.5, upper=0.5, axis="y", scale=1.0)
size = DVGeo._getNDVSpanwiseLocal()
DVCon.setDVGeo(DVGeo)
leList = [[0, 0, 0], [-radius / 2, 0, height]]
xAxis = [-1, 0, 0]
yAxis = [0, 1, 0]
DVCon.addLERadiusConstraints(leList, nSpan=5, axis=yAxis, chordDir=xAxis, scaled=False)
# DVCon.writeTecplot('cylinder_constraints.dat')
funcs = {}
DVCon.evalFunctions(funcs)
print(funcs)
handler.root_add_dict("funcs1", funcs, rtol=1e-6, atol=1e-6)
np.random.seed(0)
DVGeo.setDesignVars({"shape": (np.random.rand(size) - 0.5)})
funcs = {}
DVCon.evalFunctions(funcs)
handler.root_add_dict("funcs2", funcs, rtol=1e-6, atol=1e-6)
print(funcs)
funcsSens = {}
DVCon.evalFunctionsSens(funcsSens)
print(funcsSens)
handler.root_add_dict("funcsSens", funcsSens, rtol=1e-6, atol=1e-6)
print(funcsSens)
class PlateComponentLHS(om.ExplicitComponent):
"""Robust Bump Flow Problem, with LHS Monte Carlo Samples"""
def initialize(self):
# Need to modify this dictionary when we change the SA constants
#import pdb; pdb.set_trace()
#sys.stdout = open(os.devnull, "w")
self.aoptions = aeroOptions
self.woptions = warpOptions
self.ooptions = optOptions
self.uoptions = uqOptions
self.Pr = 0.
self.P = self.uoptions['P']
self.NS0 = self.uoptions['NS0']
# Generate FFD and DVs
if rank == 0:
rank0dvg = pf.createFFD()
else:
rank0dvg = None
self.DVGeo = comm.bcast(rank0dvg, root=0)
# starting flat mesh
meshname = self.aoptions['gridFile']
gridFile = meshname
# flow characteristics
alpha = 0.0
mach = self.ooptions['mach'] #0.95
Re = self.ooptions['Re'] #50000
Re_L = 1.0
temp = 540
arearef = 2.0
chordref = 1.0
# Spalart Allmaras model constants, to be changed in UQ (4 for now)
saconstsm = [0.41, 0.1355, 0.622, 0.66666666667]
self.saconstsb = [7.1, 0.3, 2.0, 1.0, 2.0, 1.2, 0.5, 2.0]
self.saconsts = saconstsm + self.saconstsb
self.aoptions['SAConsts'] = self.saconsts
#self.gridSol = f'{meshname}_{saconstsm}_sol'
solname = self.ooptions['prob_name']
self.gridSol = f'{solname}_sol'
# Get a set of UQ sample points (LHS)
#if self.ooptions['run_once']:
# self.sample = self.uoptions['dist']
#else
# Scatter samples, multi-point parallelism
if self.uoptions['MCTimeBudget']:
self.aps = []
self.solvers = []
self.meshes = []
self.current_samples = self.NS0
if rank == 0:
rank0sam = plate_sa_lhs.genLHS(s=self.current_samples)
else:
rank0sam = None
self.sample = comm.bcast(rank0sam, root=0)
self.cases = divide_cases(self.NS0, size)
# Scatter samples on each level, multi-point parallelism
self.samplep = self.sample[self.cases[rank]]
self.nsp = len(self.cases[rank])
# Create solvers for the preliminary data
for i in range(self.nsp):
namestr = self.gridSol + "_" + str(self.cases[rank][i])
# create meshes
self.meshes.append(
USMesh(options=self.woptions, comm=MPI.COMM_SELF))
# create aeroproblems
self.aps.append(
AeroProblem(name=namestr,
alpha=alpha,
mach=mach,
reynolds=Re,
reynoldsLength=Re_L,
T=temp,
areaRef=arearef,
chordRef=chordref,
evalFuncs=['cd']))
time.sleep(0.1) # this solves a few problems for some reason
# create solvers
self.solvers.append(
ADFLOW(options=self.aoptions, comm=MPI.COMM_SELF))
saconstsm = self.samplep[i].tolist()
self.saconsts = saconstsm + self.saconstsb
self.solvers[i].setOption('SAConsts', self.saconsts)
self.solvers[i].setDVGeo(self.DVGeo)
self.solvers[i].setMesh(self.meshes[i])
print("what up %i", str(rank))
coords = self.solvers[i].getSurfaceCoordinates(
groupName=self.solvers[i].allWallsGroup)
self.solvers[i].DVGeo.addPointSet(coords, 'coords')
# start looping over mesh levels
sumt = 0.
sumtp = 0.
Et = 0.
funcs = {}
a_init = self.DVGeo.getValues()
a_init['pnts'][:] = self.ooptions['DVInit']
dvdict = {'pnts': a_init['pnts']}
for i in range(self.nsp):
saconstsm = self.samplep[i].tolist()
self.saconsts = saconstsm + self.saconstsb
self.solvers[i].setOption('SAConsts', self.saconsts)
self.solvers[i].DVGeo.setDesignVars(dvdict)
self.aps[i].setDesignVars(dvdict)
pc0 = time.process_time()
self.solvers[i](self.aps[i])
self.solvers[i].evalFunctions(self.aps[i], funcs)
pc1 = time.process_time()
astr = self.gridSol + "_" + str(self.cases[rank][i]) + "_cd"
sumtp += (pc1 - pc0)
sumt = comm.allreduce(sumtp)
Et = sumt / self.NS0
self.NS = math.ceil(self.P / Et)
self.Pr = self.NS * Et
else:
self.NS = self.uoptions['NS']
#import pdb; pdb.set_trace()
if rank == 0:
rank0sam = plate_sa_lhs.genLHS(s=self.NS)
else:
rank0sam = None
self.sample = comm.bcast(rank0sam, root=0)
self.cases = divide_cases(self.NS, size)
self.nsp = len(self.cases[rank]) #int(ns/size) # samples per processor
#import pdb; pdb.set_trace()
self.samplep = self.sample[self.cases[
rank]] #self.sample[(rank*self.nsp):(rank*self.nsp+(self.nsp))] #shouldn't really need to "scatter" per se
#import pdb; pdb.set_trace()
#assert len(self.samplep) == self.nsp
# Actually create solvers (and aeroproblems?) (and mesh?) now
self.aps = []
self.solvers = []
self.meshes = []
#self.mesh = USMesh(options=self.woptions, comm=MPI.COMM_SELF)
for i in range(self.nsp):
namestr = self.gridSol + "_" + str(self.cases[rank][i])
# create meshes
self.meshes.append(
USMesh(options=self.woptions, comm=MPI.COMM_SELF))
# create aeroproblems
self.aps.append(
AeroProblem(name=namestr,
alpha=alpha,
mach=mach,
reynolds=Re,
reynoldsLength=Re_L,
T=temp,
areaRef=arearef,
chordRef=chordref,
evalFuncs=['cd']))
time.sleep(0.1) # this solves a few problems for some reason
# create solvers
self.solvers.append(
ADFLOW(options=self.aoptions, comm=MPI.COMM_SELF))
# if not self.ooptions['run_once']:
# saconstsm = self.samplep[i].tolist()
# else:
saconstsm = self.samplep[i].tolist()
self.saconsts = saconstsm + self.saconstsb
self.solvers[i].setOption('SAConsts', self.saconsts)
self.solvers[i].setDVGeo(self.DVGeo)
self.solvers[i].setMesh(self.meshes[i])
print("what up %i", str(rank))
coords = self.solvers[i].getSurfaceCoordinates(
groupName=self.solvers[i].allWallsGroup)
self.solvers[i].DVGeo.addPointSet(coords, 'coords')
# Set constraints, should only need one of those solvers, the meshes are all the same
self.DVCon = DVConstraints()
self.DVCon2 = DVConstraints()
self.DVCon.setDVGeo(self.solvers[0].DVGeo.getFlattenedChildren()[1])
self.DVCon2.setDVGeo(self.solvers[0].DVGeo)
self.DVCon.setSurface(self.solvers[0].getTriangulatedMeshSurface(
groupName='allSurfaces'))
# set extra group for surface area condition
self.DVCon2.setSurface(self.solvers[0].getTriangulatedMeshSurface(),
name='wall')
# DV should be same into page (not doing anything right now)
#import pdb; pdb.set_trace()
lIndex = self.solvers[0].DVGeo.getFlattenedChildren()[1].getLocalIndex(
0)
indSetA = []
indSetB = []
nXc = optOptions['NX']
self.NC = math.trunc(
((1.0 - self.ooptions['DVFraction']) * self.ooptions['NX']))
ind = [
int(nXc / 2) - int(self.NC / 2),
int(nXc / 2) + int(self.NC / 2)
]
for i in range(ind[0], ind[1]):
indSetA.append(lIndex[i, 0, 1])
indSetB.append(lIndex[i, 1, 1])
# for i in range(lIndex.shape[0]):
# indSetA.append(lIndex[i, 0, 1])
# indSetB.append(lIndex[i, 1, 1])
self.DVCon.addLinearConstraintsShape(indSetA,
indSetB,
factorA=1.0,
factorB=-1.0,
lower=0,
upper=0,
name='eqs')
# Thickness constraints (one for each active DV)
#import pdb; pdb.set_trace()
# Maximum thickness of the domain, translates to minimum thickness of bump
ub = 1.0 - self.ooptions['DCMinThick']
tcf = self.ooptions['DCThickFrac']
ra = self.ooptions['bumpBounds']
lim = self.ooptions['DCMinArea']
span = numpy.linspace(0, 1, nXc)
xc = span * (ra[1] - ra[0]) + ra[0]
#ind = range(int(nXc/2) - int(self.NC/2), int(nXc/2) + int(self.NC/2)))
ind = [
int(nXc / 2) - int(tcf * self.NC / 2),
int(nXc / 2) + int(tcf * self.NC / 2)
]
ptList = numpy.zeros([2, 3])
ptList[:, 0] = xc[ind]
ptList[:, 1] = 0.5
ptList[:, 2] = 0.5
if self.ooptions['use_area_con']:
self.DVCon2.addSurfaceAreaConstraint(lower=lim,
upper=10.,
name='sas',
surfaceName='wall')
else:
self.DVCon2.addThicknessConstraints1D(ptList,
self.NC, [0, 0, 1],
lower=0.5,
upper=ub,
name='tcs')
print("excuse me")
dummy = rank
dsum = comm.allgather(dummy)
sys.stdout = sys.__stdout__
def setup(self):
#initialize shape and set deformation points as inputs
a_init = self.solvers[0].DVGeo.getValues()
a_init['pnts'][:] = self.ooptions['DVInit']
# mult = numpy.linspace(1.0,1.5,num=int(0.5*len(a_init['pnts'])))
# mult = numpy.concatenate((mult, mult))
#if self.ooptions['run_once']:
# a_init['pnts'] = self.ooptions['ro_shape']
#a_init['pnts'] = numpy.multiply(mult, a_init['pnts'])
self.add_input('a', a_init['pnts'], desc="Bump Shape Control Points")
#self.add_input('a', 0.2, desc="Bump Shape Control Points")
if self.ooptions['use_area_con']:
self.add_output('SA', 1.0, desc='Surface Area Constraint')
else:
self.add_output('TC',
numpy.zeros(self.NC),
desc='Thickness Constraints')
self.add_output('Cd_m', 0.0, desc="Mean Drag Coefficient")
self.add_output('Cd_v', 0.0, desc="Variance Drag Coefficient")
self.add_output('Cd_r', 0.0, desc="Robust Drag Objective")
self.add_output('EQ',
numpy.zeros(int(len(a_init['pnts']) / 2)),
desc="Control Point Symmetry")
self.add_output('N1', self.NS, desc="Number of samples used")
self.add_output('Pr', self.Pr, desc="MFMC Samples at each level")
def setup_partials(self):
self.declare_partials('Cd_m', 'a', method='exact')
self.declare_partials('Cd_v', 'a', method='exact')
self.declare_partials('Cd_r', 'a', method='exact')
if self.ooptions['use_area_con']:
self.declare_partials('SA', 'a', method='exact')
else:
self.declare_partials('TC', 'a', method='exact')
self.declare_partials('EQ', 'a', method='exact')
def compute(self, inputs, outputs):
# run the bump shape model
#import pdb; pdb.set_trace()
# evaluate each sample point
#print("hello")
dvdict = {'pnts': inputs['a']}
funcs = {}
ns = self.NS
sump = 0.
musp = numpy.zeros(self.nsp)
#self.aps[0].setDesignVars(dvdict)
for i in range(self.nsp):
self.solvers[i].DVGeo.setDesignVars(dvdict)
self.aps[i].setDesignVars(dvdict)
self.solvers[i](self.aps[i])
self.solvers[i].evalFunctions(self.aps[i], funcs)
astr = self.gridSol + "_" + str(self.cases[rank][i]) + "_cd"
#import pdb; pdb.set_trace()
musp[i] = funcs[astr]
sump += funcs[astr]
# compute mean and variance
sum = comm.allreduce(sump)
mus = comm.allgather(musp)
#import pdb; pdb.set_trace()
E = sum / ns
sum2 = 0.
for i in range(len(mus)): #range(size):
for j in range(len(mus[i])): #range(self.nsp):
sum2 += (mus[i][j] - E)**2
V = sum2 / ns
self.DVCon.evalFunctions(funcs, includeLinear=True)
self.DVCon2.evalFunctions(funcs, includeLinear=True)
outputs['Cd_m'] = E
outputs['Cd_v'] = math.sqrt(V)
rho = self.uoptions['rho']
outputs['Cd_r'] = E + rho * math.sqrt(V)
if self.ooptions['use_area_con']:
outputs['SA'] = funcs['sas']
else:
outputs['TC'] = funcs['tcs']
outputs['EQ'] = funcs['eqs']
outputs['N1'] = self.NS
outputs['Pr'] = self.Pr
#outputs['Cd'] = inputs['a']*inputs['a']
def compute_partials(self, inputs, J):
dvdict = {'pnts': inputs['a']}
funcs = {}
funcSens = {}
ns = self.NS
sump = 0.
musp = numpy.zeros(self.nsp)
pmup = []
psump = numpy.zeros(len(inputs['a']))
self.aps[0].setDesignVars(dvdict)
#import pdb; pdb.set_trace()
for i in range(self.nsp):
self.solvers[i].DVGeo.setDesignVars(dvdict)
self.aps[i].setDesignVars(dvdict)
self.solvers[i].evalFunctions(self.aps[i], funcs)
self.solvers[i].evalFunctionsSens(self.aps[i], funcSens, ['cd'])
astr = self.gridSol + "_" + str(self.cases[rank][i]) + "_cd"
arr = [x * (1. / ns) for x in funcSens[astr]['pnts']]
sump += funcs[astr]
musp[i] = funcs[astr]
pmup.append(arr[0])
psump += arr[0]
sum = comm.allreduce(sump)
mus = comm.allgather(musp)
pmu = comm.allgather(pmup)
psum = comm.allreduce(psump)
#import pdb; pdb.set_trace()
#import pdb; pdb.set_trace()
# compute variance sensitivity
E = sum / ns
sum2 = 0.
psum2 = numpy.zeros(len(inputs['a']))
for i in range(len(mus)): #range(size):
for j in range(len(mus[i])): #range(self.nsp):
sum2 += (mus[i][j] - E)**2
temp = pmu[i][j] * ns - psum
arr2 = [x * 2 * (mus[i][j] - E) / ns for x in temp]
psum2 += arr2
#import pdb; pdb.set_trace()
V = sum2 / ns
#import pdb; pdb.set_trace()
self.DVCon.evalFunctionsSens(funcSens, includeLinear=True)
self.DVCon2.evalFunctionsSens(funcSens, includeLinear=True)
J['Cd_m', 'a'] = psum
J['Cd_v', 'a'] = (1. / (2 * math.sqrt(V))) * psum2
rho = self.uoptions['rho']
J['Cd_r', 'a'] = psum + rho * (1. / (2 * math.sqrt(V))) * psum2
if self.ooptions['use_area_con']:
J['SA', 'a'] = funcSens['sas']['pnts']
else:
J['TC', 'a'] = funcSens['tcs']['pnts']
J['EQ', 'a'] = funcSens['eqs']['pnts']
def initialize(self):
# Need to modify this dictionary when we change the SA constants
#import pdb; pdb.set_trace()
#sys.stdout = open(os.devnull, "w")
self.aoptions = aeroOptions
self.woptions = warpOptions
self.ooptions = optOptions
self.uoptions = uqOptions
self.Pr = 0.
self.P = self.uoptions['P']
self.NS0 = self.uoptions['NS0']
# Generate FFD and DVs
if rank == 0:
rank0dvg = pf.createFFD()
else:
rank0dvg = None
self.DVGeo = comm.bcast(rank0dvg, root=0)
# starting flat mesh
meshname = self.aoptions['gridFile']
gridFile = meshname
# flow characteristics
alpha = 0.0
mach = self.ooptions['mach'] #0.95
Re = self.ooptions['Re'] #50000
Re_L = 1.0
temp = 540
arearef = 2.0
chordref = 1.0
# Spalart Allmaras model constants, to be changed in UQ (4 for now)
saconstsm = [0.41, 0.1355, 0.622, 0.66666666667]
self.saconstsb = [7.1, 0.3, 2.0, 1.0, 2.0, 1.2, 0.5, 2.0]
self.saconsts = saconstsm + self.saconstsb
self.aoptions['SAConsts'] = self.saconsts
#self.gridSol = f'{meshname}_{saconstsm}_sol'
solname = self.ooptions['prob_name']
self.gridSol = f'{solname}_sol'
# Get a set of UQ sample points (LHS)
#if self.ooptions['run_once']:
# self.sample = self.uoptions['dist']
#else
# Scatter samples, multi-point parallelism
if self.uoptions['MCTimeBudget']:
self.aps = []
self.solvers = []
self.meshes = []
self.current_samples = self.NS0
if rank == 0:
rank0sam = plate_sa_lhs.genLHS(s=self.current_samples)
else:
rank0sam = None
self.sample = comm.bcast(rank0sam, root=0)
self.cases = divide_cases(self.NS0, size)
# Scatter samples on each level, multi-point parallelism
self.samplep = self.sample[self.cases[rank]]
self.nsp = len(self.cases[rank])
# Create solvers for the preliminary data
for i in range(self.nsp):
namestr = self.gridSol + "_" + str(self.cases[rank][i])
# create meshes
self.meshes.append(
USMesh(options=self.woptions, comm=MPI.COMM_SELF))
# create aeroproblems
self.aps.append(
AeroProblem(name=namestr,
alpha=alpha,
mach=mach,
reynolds=Re,
reynoldsLength=Re_L,
T=temp,
areaRef=arearef,
chordRef=chordref,
evalFuncs=['cd']))
time.sleep(0.1) # this solves a few problems for some reason
# create solvers
self.solvers.append(
ADFLOW(options=self.aoptions, comm=MPI.COMM_SELF))
saconstsm = self.samplep[i].tolist()
self.saconsts = saconstsm + self.saconstsb
self.solvers[i].setOption('SAConsts', self.saconsts)
self.solvers[i].setDVGeo(self.DVGeo)
self.solvers[i].setMesh(self.meshes[i])
print("what up %i", str(rank))
coords = self.solvers[i].getSurfaceCoordinates(
groupName=self.solvers[i].allWallsGroup)
self.solvers[i].DVGeo.addPointSet(coords, 'coords')
# start looping over mesh levels
sumt = 0.
sumtp = 0.
Et = 0.
funcs = {}
a_init = self.DVGeo.getValues()
a_init['pnts'][:] = self.ooptions['DVInit']
dvdict = {'pnts': a_init['pnts']}
for i in range(self.nsp):
saconstsm = self.samplep[i].tolist()
self.saconsts = saconstsm + self.saconstsb
self.solvers[i].setOption('SAConsts', self.saconsts)
self.solvers[i].DVGeo.setDesignVars(dvdict)
self.aps[i].setDesignVars(dvdict)
pc0 = time.process_time()
self.solvers[i](self.aps[i])
self.solvers[i].evalFunctions(self.aps[i], funcs)
pc1 = time.process_time()
astr = self.gridSol + "_" + str(self.cases[rank][i]) + "_cd"
sumtp += (pc1 - pc0)
sumt = comm.allreduce(sumtp)
Et = sumt / self.NS0
self.NS = math.ceil(self.P / Et)
self.Pr = self.NS * Et
else:
self.NS = self.uoptions['NS']
#import pdb; pdb.set_trace()
if rank == 0:
rank0sam = plate_sa_lhs.genLHS(s=self.NS)
else:
rank0sam = None
self.sample = comm.bcast(rank0sam, root=0)
self.cases = divide_cases(self.NS, size)
self.nsp = len(self.cases[rank]) #int(ns/size) # samples per processor
#import pdb; pdb.set_trace()
self.samplep = self.sample[self.cases[
rank]] #self.sample[(rank*self.nsp):(rank*self.nsp+(self.nsp))] #shouldn't really need to "scatter" per se
#import pdb; pdb.set_trace()
#assert len(self.samplep) == self.nsp
# Actually create solvers (and aeroproblems?) (and mesh?) now
self.aps = []
self.solvers = []
self.meshes = []
#self.mesh = USMesh(options=self.woptions, comm=MPI.COMM_SELF)
for i in range(self.nsp):
namestr = self.gridSol + "_" + str(self.cases[rank][i])
# create meshes
self.meshes.append(
USMesh(options=self.woptions, comm=MPI.COMM_SELF))
# create aeroproblems
self.aps.append(
AeroProblem(name=namestr,
alpha=alpha,
mach=mach,
reynolds=Re,
reynoldsLength=Re_L,
T=temp,
areaRef=arearef,
chordRef=chordref,
evalFuncs=['cd']))
time.sleep(0.1) # this solves a few problems for some reason
# create solvers
self.solvers.append(
ADFLOW(options=self.aoptions, comm=MPI.COMM_SELF))
# if not self.ooptions['run_once']:
# saconstsm = self.samplep[i].tolist()
# else:
saconstsm = self.samplep[i].tolist()
self.saconsts = saconstsm + self.saconstsb
self.solvers[i].setOption('SAConsts', self.saconsts)
self.solvers[i].setDVGeo(self.DVGeo)
self.solvers[i].setMesh(self.meshes[i])
print("what up %i", str(rank))
coords = self.solvers[i].getSurfaceCoordinates(
groupName=self.solvers[i].allWallsGroup)
self.solvers[i].DVGeo.addPointSet(coords, 'coords')
# Set constraints, should only need one of those solvers, the meshes are all the same
self.DVCon = DVConstraints()
self.DVCon2 = DVConstraints()
self.DVCon.setDVGeo(self.solvers[0].DVGeo.getFlattenedChildren()[1])
self.DVCon2.setDVGeo(self.solvers[0].DVGeo)
self.DVCon.setSurface(self.solvers[0].getTriangulatedMeshSurface(
groupName='allSurfaces'))
# set extra group for surface area condition
self.DVCon2.setSurface(self.solvers[0].getTriangulatedMeshSurface(),
name='wall')
# DV should be same into page (not doing anything right now)
#import pdb; pdb.set_trace()
lIndex = self.solvers[0].DVGeo.getFlattenedChildren()[1].getLocalIndex(
0)
indSetA = []
indSetB = []
nXc = optOptions['NX']
self.NC = math.trunc(
((1.0 - self.ooptions['DVFraction']) * self.ooptions['NX']))
ind = [
int(nXc / 2) - int(self.NC / 2),
int(nXc / 2) + int(self.NC / 2)
]
for i in range(ind[0], ind[1]):
indSetA.append(lIndex[i, 0, 1])
indSetB.append(lIndex[i, 1, 1])
# for i in range(lIndex.shape[0]):
# indSetA.append(lIndex[i, 0, 1])
# indSetB.append(lIndex[i, 1, 1])
self.DVCon.addLinearConstraintsShape(indSetA,
indSetB,
factorA=1.0,
factorB=-1.0,
lower=0,
upper=0,
name='eqs')
# Thickness constraints (one for each active DV)
#import pdb; pdb.set_trace()
# Maximum thickness of the domain, translates to minimum thickness of bump
ub = 1.0 - self.ooptions['DCMinThick']
tcf = self.ooptions['DCThickFrac']
ra = self.ooptions['bumpBounds']
lim = self.ooptions['DCMinArea']
span = numpy.linspace(0, 1, nXc)
xc = span * (ra[1] - ra[0]) + ra[0]
#ind = range(int(nXc/2) - int(self.NC/2), int(nXc/2) + int(self.NC/2)))
ind = [
int(nXc / 2) - int(tcf * self.NC / 2),
int(nXc / 2) + int(tcf * self.NC / 2)
]
ptList = numpy.zeros([2, 3])
ptList[:, 0] = xc[ind]
ptList[:, 1] = 0.5
ptList[:, 2] = 0.5
if self.ooptions['use_area_con']:
self.DVCon2.addSurfaceAreaConstraint(lower=lim,
upper=10.,
name='sas',
surfaceName='wall')
else:
self.DVCon2.addThicknessConstraints1D(ptList,
self.NC, [0, 0, 1],
lower=0.5,
upper=ub,
name='tcs')
print("excuse me")
dummy = rank
dsum = comm.allgather(dummy)
sys.stdout = sys.__stdout__
def initialize(self):
# Need to modify this dictionary when we change the SA constants
sys.stdout = open(os.devnull, "w")
self.aoptions = aeroOptions
self.woptions = warpOptions
self.ooptions = optOptions
# Generate FFD and DVs
self.DVGeo = pf.createFFD()
# starting flat mesh
meshname = self.aoptions['gridFile']
gridFile = meshname
# flow characteristics
alpha = 0.0
mach = self.ooptions['mach']#0.95
Re = self.ooptions['Re']#50000
Re_L = 1.0
temp = 540
arearef = 2.0
chordref = 1.0
# Spalart Allmaras model constants, to be changed in UQ
saconstsm = [0.41, 0.1355, 0.622, 0.66666666667, 7.1, 0.3, 2.0]
self.saconsts = saconstsm + [1.0, 2.0, 1.2, 0.5, 2.0]
self.aoptions['SAConsts'] = self.saconsts
#self.gridSol = f'{meshname}_{saconstsm}_sol'
solname = self.ooptions['prob_name']
self.gridSol = f'{solname}_sol'
# Aerodynamic problem description
self.ap = AeroProblem(name=self.gridSol, alpha=alpha, mach=mach, reynolds=Re, reynoldsLength=Re_L, T=temp, areaRef=arearef, chordRef=chordref,
evalFuncs=['cd'])
# Create solver
self.CFDSolver = ADFLOW(options=self.aoptions, comm=MPI.COMM_WORLD)
self.CFDSolver.setDVGeo(self.DVGeo)
# Set up mesh warping
self.mesh = USMesh(options=self.woptions, comm=MPI.COMM_WORLD)
self.CFDSolver.setMesh(self.mesh)
# Try setting the DVGeo coordinates here
coords = self.CFDSolver.getSurfaceCoordinates(groupName=self.CFDSolver.allWallsGroup)
self.CFDSolver.DVGeo.addPointSet(coords, 'coords')
self.CFDSolver.DVGeo.getFlattenedChildren()[1].writePlot3d("ffdp_opt_def.xyz")
# Set constraints
self.DVCon = DVConstraints()
self.DVCon2 = DVConstraints()
self.DVCon.setDVGeo(self.CFDSolver.DVGeo.getFlattenedChildren()[1])
self.DVCon2.setDVGeo(self.CFDSolver.DVGeo)
self.DVCon.setSurface(self.CFDSolver.getTriangulatedMeshSurface(groupName='allSurfaces'))
# set extra group for surface area condition
self.DVCon2.setSurface(self.CFDSolver.getTriangulatedMeshSurface(), name='wall')
# DV should be same into page (not doing anything right now)
#import pdb; pdb.set_trace()
lIndex = self.CFDSolver.DVGeo.getFlattenedChildren()[1].getLocalIndex(0)
indSetA = []
indSetB = []
nXc = optOptions['NX']
self.NC = math.trunc(((1.0 - self.ooptions['DVFraction'])*self.ooptions['NX']))
ind = [int(nXc/2) - int(self.NC/2), int(nXc/2) + int(self.NC/2)]
for i in range(ind[0], ind[1]):
indSetA.append(lIndex[i, 0, 1])
indSetB.append(lIndex[i, 1, 1])
# for i in range(lIndex.shape[0]):
# indSetA.append(lIndex[i, 0, 1])
# indSetB.append(lIndex[i, 1, 1])
self.DVCon.addLinearConstraintsShape(indSetA, indSetB, factorA=1.0, factorB=-1.0, lower=0, upper=0, name='eqs')
# Thickness constraints (one for each active DV)
#import pdb; pdb.set_trace()
# Maximum thickness of the domain, translates to minimum thickness of bump
ub = 1.0 - self.ooptions['DCMinThick']
tcf = self.ooptions['DCThickFrac']
ra = self.ooptions['bumpBounds']
lim = self.ooptions['DCMinArea']
span = numpy.linspace(0, 1, nXc)
xc = span * (ra[1] - ra[0]) + ra[0]
#ind = range(int(nXc/2) - int(self.NC/2), int(nXc/2) + int(self.NC/2)))
ind = [int(nXc/2) - int(tcf*self.NC/2), int(nXc/2) + int(tcf*self.NC/2)]
ptList = numpy.zeros([2, 3])
ptList[:,0] = xc[ind]
ptList[:,1] = 0.5
ptList[:,2] = 0.5
if self.ooptions['use_area_con']:
self.DVCon2.addSurfaceAreaConstraint(lower=lim, upper=10., name='sas', surfaceName='wall')
else:
self.DVCon2.addThicknessConstraints1D(ptList, self.NC, [0,0,1], lower=0.5, upper=ub, name='tcs')
sys.stdout = sys.__stdout__
def initialize(self):
# Need to modify this dictionary when we change the SA constants
#import pdb; pdb.set_trace()
#sys.stdout = open(os.devnull, "w")
self.aoptions = aeroOptions
self.woptions = warpOptions
self.ooptions = optOptions
self.uoptions = uqOptions
self.Pr = 0.
# Generate FFD and DVs
if rank == 0:
rank0dvg = pf.createFFD()
else:
rank0dvg = None
self.DVGeo = comm.bcast(rank0dvg, root=0)
# Get a full list of every mesh name we have, assume they are ordered properly by level
self.meshnames = self.uoptions['gridFileLevels']
self.Lmax = len(self.meshnames) #as many levels as we have meshes
self.mord = [*range(self.Lmax)]
self.mord.reverse()
if self.Lmax < 3:
raise ValueError('Not enough meshes available, ' + self.Lmax +
' < 3')
# Spalart Allmaras model constants, to be changed in UQ (4 for now)
saconstsm = [0.41, 0.1355, 0.622, 0.66666666667]
self.saconstsb = [7.1, 0.3, 2.0, 1.0, 2.0, 1.2, 0.5, 2.0]
self.saconsts = saconstsm + self.saconstsb
self.aoptions['SAConsts'] = self.saconsts
#self.gridSol = f'{meshname}_{saconstsm}_sol'
solname = self.ooptions['prob_name']
self.gridSol = f'{solname}_sol'
self.cases = []
#self.nsp = [] #keep track per level
self.samplep = []
self.naddedtot = []
for i in range(self.Lmax):
self.naddedtot.append(0)
self.aps = []
self.solvers = []
self.meshes = []
self.NS0 = self.uoptions['NS0']
self.current_samples = self.NS0 * self.Lmax
self.N1 = None
self.a1 = None
self.P = self.uoptions['P']
##########
# call distribute samples here?
if not self.uoptions['use-predetermined-samples']:
self.MFMC()
else:
self.N1 = self.uoptions['predet-N1']
self.a1 = self.uoptions['predet-a1']
self.dist_samples()
##########
# Set constraints, should only need one of those solvers, the meshes are all the same
if rank == 0:
self.DVCon = DVConstraints()
self.DVCon2 = DVConstraints()
self.DVCon.setDVGeo(
self.solvers[0][0].DVGeo.getFlattenedChildren()[1])
self.DVCon2.setDVGeo(self.solvers[0][0].DVGeo)
self.DVCon.setSurface(
self.solvers[0][0].getTriangulatedMeshSurface(
groupName='allSurfaces'))
# set extra group for surface area condition
self.DVCon2.setSurface(
self.solvers[0][0].getTriangulatedMeshSurface(), name='wall')
# DV should be same into page (not doing anything right now)
#import pdb; pdb.set_trace()
lIndex = self.solvers[0][0].DVGeo.getFlattenedChildren(
)[1].getLocalIndex(0)
indSetA = []
indSetB = []
nXc = optOptions['NX']
self.NC = math.trunc(
((1.0 - self.ooptions['DVFraction']) * self.ooptions['NX']))
ind = [
int(nXc / 2) - int(self.NC / 2),
int(nXc / 2) + int(self.NC / 2)
]
for i in range(ind[0], ind[1]):
indSetA.append(lIndex[i, 0, 1])
indSetB.append(lIndex[i, 1, 1])
# for i in range(lIndex.shape[0]):
# indSetA.append(lIndex[i, 0, 1])
# indSetB.append(lIndex[i, 1, 1])
self.DVCon.addLinearConstraintsShape(indSetA,
indSetB,
factorA=1.0,
factorB=-1.0,
lower=0,
upper=0,
name='eqs')
# Thickness constraints (one for each active DV)
#import pdb; pdb.set_trace()
# Maximum thickness of the domain, translates to minimum thickness of bump
ub = 1.0 - self.ooptions['DCMinThick']
tcf = self.ooptions['DCThickFrac']
ra = self.ooptions['bumpBounds']
lim = self.ooptions['DCMinArea']
span = numpy.linspace(0, 1, nXc)
xc = span * (ra[1] - ra[0]) + ra[0]
#ind = range(int(nXc/2) - int(self.NC/2), int(nXc/2) + int(self.NC/2)))
ind = [
int(nXc / 2) - int(tcf * self.NC / 2),
int(nXc / 2) + int(tcf * self.NC / 2)
]
ptList = numpy.zeros([2, 3])
ptList[:, 0] = xc[ind]
ptList[:, 1] = 0.5
ptList[:, 2] = 0.5
if self.ooptions['use_area_con']:
self.DVCon2.addSurfaceAreaConstraint(lower=lim,
upper=10.,
name='sas',
surfaceName='wall')
else:
self.DVCon2.addThicknessConstraints1D(ptList,
self.NC, [0, 0, 1],
lower=0.5,
upper=ub,
name='tcs')
dummy = rank
dsum = comm.allgather(dummy)
sys.stdout = sys.__stdout__
def test_1(self, train=False, refDeriv=False):
refFile = os.path.join(self.base_path, 'ref/test_Cylinder_01.ref')
with BaseRegTest(refFile, train=train) as handler:
handler.root_print("Test 1: Basic FFD, global DVs")
radius = 1.0
height = 10.0
DVCon = DVConstraints()
surf = self.make_cylinder_mesh(radius, height)
DVCon.setSurface(surf)
# DVCon.writeSurfaceTecplot('cylinder_surface.dat')
ffd_name = os.path.join(self.base_path,
'../inputFiles/cylinder_ffd.xyz')
self.make_ffd(ffd_name, radius, height)
DVGeo = DVGeometry(ffd_name)
nAxPts = DVGeo.addRefAxis('thru',
xFraction=0.5,
alignIndex='i',
raySize=1.0)
def scale_circle(val, geo):
for i in range(nAxPts):
geo.scale['thru'].coef[i] = val[0]
DVGeo.addGeoDVGlobal('scale_circle', func=scale_circle, value=[1])
DVCon.setDVGeo(DVGeo)
leList = [[0, 0, 0], [-radius / 2, 0, height]]
xAxis = [-1, 0, 0]
yAxis = [0, 1, 0]
DVCon.addLERadiusConstraints(leList,
nSpan=5,
axis=yAxis,
chordDir=xAxis,
scaled=False)
# DVCon.writeTecplot('cylinder_constraints.dat')
funcs = {}
DVCon.evalFunctions(funcs)
print(funcs)
handler.root_add_dict(funcs, 1e-6, 1e-6)
DVGeo.setDesignVars({'scale_circle': 0.5})
funcs = {}
DVCon.evalFunctions(funcs)
handler.root_add_dict(funcs, 1e-6, 1e-6)
print(funcs)
funcsSens = {}
DVCon.evalFunctionsSens(funcsSens)
handler.root_add_dict(funcsSens, 1e-6, 1e-6)
print(funcsSens)
geo.rot_z["wing"].coef[i] = val[i - 1]
DVGeo.addGeoDVGlobal(dvName="twist", value=[0] * nTwist, func=twist, lower=-10, upper=10, scale=0.01)
# Set up local design variables
DVGeo.addGeoDVLocal("local", lower=-0.5, upper=0.5, axis="y", scale=1)
# Add DVGeo object to CFD solver
CFDSolver.setDVGeo(DVGeo)
# rst dvgeo (end)
# ======================================================================
# DVConstraint Setup
# ======================================================================
# rst dvcon (beg)
DVCon = DVConstraints()
DVCon.setDVGeo(DVGeo)
# Only ADflow has the getTriangulatedSurface Function
DVCon.setSurface(CFDSolver.getTriangulatedMeshSurface())
# Volume constraints
leList = [[0.01, 0, 0.001], [7.51, 0, 13.99]]
teList = [[4.99, 0, 0.001], [8.99, 0, 13.99]]
DVCon.addVolumeConstraint(leList, teList, 20, 20, lower=1.0)
# Thickness constraints
DVCon.addThicknessConstraints2D(leList, teList, 10, 10, lower=1.0)
# Le/Te constraints
DVCon.addLeTeConstraints(0, "iLow")
func=twist,
lower=-10,
upper=10,
scale=0.01)
# Set up local design variables
DVGeo.addGeoDVLocal('local', lower=-0.5, upper=0.5, axis='y', scale=1)
# Add DVGeo object to CFD solver
CFDSolver.setDVGeo(DVGeo)
#rst dvgeo (end)
# ======================================================================
# DVConstraint Setup
# ======================================================================
#rst dvcon (beg)
DVCon = DVConstraints()
DVCon.setDVGeo(DVGeo)
# Only ADflow has the getTriangulatedSurface Function
DVCon.setSurface(CFDSolver.getTriangulatedMeshSurface())
# Volume constraints
leList = [[0.01, 0, 0.001], [7.51, 0, 13.99]]
teList = [[4.99, 0, 0.001], [8.99, 0, 13.99]]
DVCon.addVolumeConstraint(leList, teList, 20, 20, lower=1.0)
# Thickness constraints
DVCon.addThicknessConstraints2D(leList, teList, 10, 10, lower=1.0)
# Le/Te constraints
DVCon.addLeTeConstraints(0, 'iLow')
def test_triangulatedSurface_intersected_2DVGeos(self, train=False, refDeriv=False):
refFile = os.path.join(self.base_path, "ref/test_DVConstraints_triangulatedSurface_intersected_2DVGeos.ref")
with BaseRegTest(refFile, train=train) as handler:
meshFile = os.path.join(self.base_path, "../../input_files/bwb.stl")
objFile = os.path.join(self.base_path, "../../input_files/blob_bwb_wing.stl")
ffdFile = os.path.join(self.base_path, "../../input_files/bwb.xyz")
testMesh = mesh.Mesh.from_file(meshFile)
testObj = mesh.Mesh.from_file(objFile)
# test mesh dim 0 is triangle index
# dim 1 is each vertex of the triangle
# dim 2 is x, y, z dimension
# create a DVGeo object with a few local thickness variables
DVGeo1 = DVGeometry(ffdFile)
nRefAxPts = DVGeo1.addRefAxis("wing", xFraction=0.25, alignIndex="k")
self.nTwist = nRefAxPts - 1
def twist(val, geo):
for i in range(1, nRefAxPts):
geo.rot_z["wing"].coef[i] = val[i - 1]
DVGeo1.addGlobalDV(dvName="twist", value=[0] * self.nTwist, func=twist, lower=-10, upper=10, scale=1)
DVGeo1.addLocalDV("local", lower=-0.5, upper=0.5, axis="y", scale=1)
# create a DVGeo object with a few local thickness variables
DVGeo2 = DVGeometry(ffdFile, name="blobdvgeo")
DVGeo2.addLocalDV("local_2", lower=-0.5, upper=0.5, axis="y", scale=1)
# check that DVGeos with duplicate var names are not allowed
DVGeo3 = DVGeometry(ffdFile)
DVGeo3.addLocalDV("local", lower=-0.5, upper=0.5, axis="y", scale=1)
# create a DVConstraints object for the wing
DVCon = DVConstraints()
DVCon.setDVGeo(DVGeo1)
DVCon.setDVGeo(DVGeo2, name="second")
with self.assertRaises(ValueError):
DVCon.setDVGeo(DVGeo3, name="third")
p0 = testMesh.vectors[:, 0, :]
v1 = testMesh.vectors[:, 1, :] - p0
v2 = testMesh.vectors[:, 2, :] - p0
DVCon.setSurface([p0, v1, v2], addToDVGeo=True)
p0b = testObj.vectors[:, 0, :]
v1b = testObj.vectors[:, 1, :] - p0b
v2b = testObj.vectors[:, 2, :] - p0b
p0b = p0b + np.array([0.0, 0.3, 0.0])
DVCon.setSurface([p0b, v1b, v2b], name="blob", addToDVGeo=True, DVGeoName="second")
DVCon.addTriangulatedSurfaceConstraint("default", "default", "blob", "second", rho=10.0, addToPyOpt=True)
funcs = {}
DVCon.evalFunctions(funcs, includeLinear=True)
handler.root_add_dict("funcs_base", funcs, rtol=1e-6, atol=1e-6)
funcsSens = {}
DVCon.evalFunctionsSens(funcsSens, includeLinear=True)
# regress the derivatives
handler.root_add_dict("derivs_base", funcsSens, rtol=1e-6, atol=1e-6)
# FD check DVGeo1
funcsSensFD = evalFunctionsSensFD(DVGeo1, DVCon, fdstep=1e-3)
at_least_one_var = False
for outkey in funcs.keys():
for inkey in DVGeo1.getValues().keys():
analytic = funcsSens[outkey][inkey]
fd = funcsSensFD[outkey][inkey]
handler.assert_allclose(analytic, fd, name="finite_diff_check", rtol=1e-3, atol=1e-3)
# make sure there are actually checks happening
self.assertTrue(np.abs(np.sum(fd)) > 1e-10)
at_least_one_var = True
self.assertTrue(at_least_one_var)
# FD check DVGeo2
funcsSensFD = evalFunctionsSensFD(DVGeo2, DVCon, fdstep=1e-3)
at_least_one_var = False
for outkey in funcs.keys():
for inkey in DVGeo2.getValues().keys():
analytic = funcsSens[outkey][inkey]
fd = funcsSensFD[outkey][inkey]
handler.assert_allclose(analytic, fd, name="finite_diff_check", rtol=1e-3, atol=1e-3)
self.assertTrue(np.abs(np.sum(fd)) > 1e-10)
at_least_one_var = True
self.assertTrue(at_least_one_var)
def generate_dvgeo_dvcon(self, geometry, addToDVGeo=False, intersected=False):
"""
This function creates the DVGeometry and DVConstraints objects for each geometry used in this class.
The C172 wing represents a typical use case with twist and shape variables.
The rectangular box is primarily used to test unscaled constraint function
values against known values for thickness, volume, and surface area.
The BWB is used for the triangulated surface and volume constraint tests.
The RAE 2822 wing is used for the curvature constraint test.
"""
if geometry == "c172":
meshFile = os.path.join(self.base_path, "../../input_files/c172.stl")
ffdFile = os.path.join(self.base_path, "../../input_files/c172.xyz")
xFraction = 0.25
meshScale = 1e-3
elif geometry == "box":
meshFile = os.path.join(self.base_path, "../../input_files/2x1x8_rectangle.stl")
ffdFile = os.path.join(self.base_path, "../../input_files/2x1x8_rectangle.xyz")
xFraction = 0.5
meshScale = 1
elif geometry == "bwb":
meshFile = os.path.join(self.base_path, "../../input_files/bwb.stl")
ffdFile = os.path.join(self.base_path, "../../input_files/bwb.xyz")
xFraction = 0.25
meshScale = 1
elif geometry == "rae2822":
ffdFile = os.path.join(self.base_path, "../../input_files/deform_geometry_ffd.xyz")
xFraction = 0.25
DVGeo = DVGeometry(ffdFile, child=self.child)
DVCon = DVConstraints()
nRefAxPts = DVGeo.addRefAxis("wing", xFraction=xFraction, alignIndex="k")
self.nTwist = nRefAxPts - 1
if self.child:
parentFFD = os.path.join(self.base_path, "../../input_files/parent.xyz")
self.parentDVGeo = DVGeometry(parentFFD)
self.parentDVGeo.addChild(DVGeo)
DVCon.setDVGeo(self.parentDVGeo)
else:
DVCon.setDVGeo(DVGeo)
# Add design variables
def twist(val, geo):
for i in range(1, nRefAxPts):
geo.rot_z["wing"].coef[i] = val[i - 1]
DVGeo.addGlobalDV(dvName="twist", value=[0] * self.nTwist, func=twist, lower=-10, upper=10, scale=1)
DVGeo.addLocalDV("local", lower=-0.5, upper=0.5, axis="y", scale=1)
# RAE 2822 does not have a DVCon surface so we just return
if geometry == "rae2822":
return DVGeo, DVCon
# Get the mesh from the STL
testMesh = mesh.Mesh.from_file(meshFile)
# dim 0 is triangle index
# dim 1 is each vertex of the triangle
# dim 2 is x, y, z dimension
p0 = testMesh.vectors[:, 0, :] * meshScale
v1 = testMesh.vectors[:, 1, :] * meshScale - p0
v2 = testMesh.vectors[:, 2, :] * meshScale - p0
DVCon.setSurface([p0, v1, v2], addToDVGeo=addToDVGeo)
# Add the blob surface for the BWB
if geometry == "bwb":
objFile = os.path.join(self.base_path, "../../input_files/blob_bwb_wing.stl")
testObj = mesh.Mesh.from_file(objFile)
p0b = testObj.vectors[:, 0, :]
v1b = testObj.vectors[:, 1, :] - p0b
v2b = testObj.vectors[:, 2, :] - p0b
if intersected:
p0b = p0b + np.array([0.0, 0.3, 0.0])
DVCon.setSurface([p0b, v1b, v2b], name="blob")
return DVGeo, DVCon
class PlateComponentMLMC(om.ExplicitComponent):
"""Robust Bump Flow Problem, with LHS Multi Level Monte Carlo Samples"""
def initialize(self):
# Need to modify this dictionary when we change the SA constants
#import pdb; pdb.set_trace()
sys.stdout = open(os.devnull, "w")
self.aoptions = aeroOptions
self.woptions = warpOptions
self.ooptions = optOptions
self.uoptions = uqOptions
# Generate FFD and DVs
if rank == 0:
rank0dvg = pf.createFFD()
else:
rank0dvg = None
self.DVGeo = comm.bcast(rank0dvg, root=0)
# Get a full list of every mesh name we have, assume they are ordered properly by level
self.meshnames = self.uoptions['gridFileLevels']
self.Lmax = len(self.meshnames) #as many levels as we have meshes
if self.Lmax < 3:
raise ValueError('Not enough meshes available, ' + self.Lmax +
' < 3')
# Spalart Allmaras model constants, to be changed in UQ (4 for now)
saconstsm = [0.41, 0.1355, 0.622, 0.66666666667]
self.saconstsb = [7.1, 0.3, 2.0, 1.0, 2.0, 1.2, 0.5, 2.0]
self.saconsts = saconstsm + self.saconstsb
self.aoptions['SAConsts'] = self.saconsts
#self.gridSol = f'{meshname}_{saconstsm}_sol'
solname = self.ooptions['prob_name']
self.gridSol = f'{solname}_sol'
self.cases = []
self.nsp = [] #keep track per level
self.samplep = []
self.naddedtot = []
for i in range(self.Lmax):
self.naddedtot.append(0)
self.aps = []
self.solvers = []
self.meshes = []
self.NS0 = self.uoptions['NS0']
self.current_samples = self.NS0 * self.Lmax
self.N1 = None
##########
# call distribute samples here?
if not self.uoptions['use-predetermined-samples']:
self.MLMC()
else:
self.N1 = self.uoptions['predet-N1']
self.dist_samples()
##########
# Set constraints, should only need one of those solvers, the meshes are all the same
if rank == 0:
self.DVCon = DVConstraints()
self.DVCon2 = DVConstraints()
self.DVCon.setDVGeo(
self.solvers[self.Lmax - 1][0].DVGeo.getFlattenedChildren()[1])
self.DVCon2.setDVGeo(self.solvers[self.Lmax - 1][0].DVGeo)
self.DVCon.setSurface(
self.solvers[self.Lmax - 1][0].getTriangulatedMeshSurface(
groupName='allSurfaces'))
# set extra group for surface area condition
self.DVCon2.setSurface(
self.solvers[self.Lmax - 1][0].getTriangulatedMeshSurface(),
name='wall')
# DV should be same into page (not doing anything right now)
#import pdb; pdb.set_trace()
lIndex = self.solvers[
self.Lmax -
1][0].DVGeo.getFlattenedChildren()[1].getLocalIndex(0)
indSetA = []
indSetB = []
nXc = optOptions['NX']
self.NC = math.trunc(
((1.0 - self.ooptions['DVFraction']) * self.ooptions['NX']))
ind = [
int(nXc / 2) - int(self.NC / 2),
int(nXc / 2) + int(self.NC / 2)
]
for i in range(ind[0], ind[1]):
indSetA.append(lIndex[i, 0, 1])
indSetB.append(lIndex[i, 1, 1])
# for i in range(lIndex.shape[0]):
# indSetA.append(lIndex[i, 0, 1])
# indSetB.append(lIndex[i, 1, 1])
self.DVCon.addLinearConstraintsShape(indSetA,
indSetB,
factorA=1.0,
factorB=-1.0,
lower=0,
upper=0,
name='eqs')
# Thickness constraints (one for each active DV)
#import pdb; pdb.set_trace()
# Maximum thickness of the domain, translates to minimum thickness of bump
ub = 1.0 - self.ooptions['DCMinThick']
tcf = self.ooptions['DCThickFrac']
ra = self.ooptions['bumpBounds']
lim = self.ooptions['DCMinArea']
span = numpy.linspace(0, 1, nXc)
xc = span * (ra[1] - ra[0]) + ra[0]
#ind = range(int(nXc/2) - int(self.NC/2), int(nXc/2) + int(self.NC/2)))
ind = [
int(nXc / 2) - int(tcf * self.NC / 2),
int(nXc / 2) + int(tcf * self.NC / 2)
]
ptList = numpy.zeros([2, 3])
ptList[:, 0] = xc[ind]
ptList[:, 1] = 0.5
ptList[:, 2] = 0.5
if self.ooptions['use_area_con']:
self.DVCon2.addSurfaceAreaConstraint(lower=lim,
upper=10.,
name='sas',
surfaceName='wall')
else:
self.DVCon2.addThicknessConstraints1D(ptList,
self.NC, [0, 0, 1],
lower=0.5,
upper=ub,
name='tcs')
dummy = rank
dsum = comm.allgather(dummy)
sys.stdout = sys.__stdout__
def setup(self):
#initialize shape and set deformation points as inputs
a_init = self.DVGeo.getValues()
a_init['pnts'][:] = self.ooptions['DVInit']
# mult = numpy.linspace(1.0,1.5,num=int(0.5*len(a_init['pnts'])))
# mult = numpy.concatenate((mult, mult))
#if self.ooptions['run_once']:
# a_init['pnts'] = self.ooptions['ro_shape']
#a_init['pnts'] = numpy.multiply(mult, a_init['pnts'])
self.add_input('a', a_init['pnts'], desc="Bump Shape Control Points")
#self.add_input('a', 0.2, desc="Bump Shape Control Points")
if self.ooptions['use_area_con']:
self.add_output('SA', 1.0, desc='Surface Area Constraint')
else:
self.add_output('TC',
numpy.zeros(self.NC),
desc='Thickness Constraints')
self.add_output('Cd_m', 0.0, desc="Mean Drag Coefficient")
self.add_output('Cd_v', 0.0, desc="Variance Drag Coefficient")
self.add_output('Cd_r', 0.0, desc="Robust Drag Objective")
self.add_output('EQ',
numpy.zeros(int(len(a_init['pnts']) / 2)),
desc="Control Point Symmetry")
self.add_output('N1', self.N1, desc="MLMC Samples at each level")
def setup_partials(self):
self.declare_partials('Cd_m', 'a', method='exact')
self.declare_partials('Cd_v', 'a', method='exact')
self.declare_partials('Cd_r', 'a', method='exact')
if self.ooptions['use_area_con']:
self.declare_partials('SA', 'a', method='exact')
else:
self.declare_partials('TC', 'a', method='exact')
self.declare_partials('EQ', 'a', method='exact')
def compute(self, inputs, outputs):
# run the bump shape model
#import pdb; pdb.set_trace()
dvdict = {'pnts': inputs['a']}
ntot = self.current_samples
nslp = []
nslt = []
for k in range(self.Lmax):
nslp.append(len(self.cases[k][rank]))
nslt.append(sum([len(self.cases[k][x]) for x in range(size)]))
funcs = {}
sump = []
musp = []
sum1 = []
mus = []
sumpm = []
muspm = []
summ = []
musm = []
E = numpy.zeros(self.Lmax)
V = numpy.zeros(self.Lmax)
for k in range(self.Lmax):
sump.append(0.0)
musp.append(numpy.zeros(nslp[k]))
sumpm.append(0.)
muspm.append(numpy.zeros(nslp[k]))
for i in range(nslp[k]):
saconstsm = self.samplep[k][i].tolist()
self.saconsts = saconstsm + self.saconstsb
self.solvers[k][i].setOption('SAConsts', self.saconsts)
self.solvers[k][i].DVGeo.setDesignVars(dvdict)
self.aps[k][i].setDesignVars(dvdict)
self.solvers[k][i](self.aps[k][i])
self.solvers[k][i].evalFunctions(self.aps[k][i], funcs)
astr = self.gridSol + "_" + str(self.cases[k][rank][i]) + "_cd"
musp[k][i] = funcs[astr]
sump[k] += funcs[astr]
if k > 0:
self.solvers[k][i + nslp[k]].setOption(
'SAConsts', self.saconsts)
self.solvers[k][i + nslp[k]].DVGeo.setDesignVars(dvdict)
self.aps[k][i + nslp[k]].setDesignVars(dvdict)
self.solvers[k][i + nslp[k]](self.aps[k][i + nslp[k]])
self.solvers[k][i + nslp[k]].evalFunctions(
self.aps[k][i + nslp[k]], funcs)
astr = self.gridSol + "_" + str(
self.cases[k][rank][i]) + "_m_cd"
muspm[k][i] = -funcs[astr]
sumpm[k] += -funcs[astr]
# compute mean and variance
for k in range(self.Lmax):
sum1.append(comm.allreduce(sump[k]))
mus.append(comm.allgather(musp[k]))
summ.append(comm.allreduce(sumpm[k]))
musm.append(comm.allgather(muspm[k]))
#import pdb; pdb.set_trace()
E[k] = (sum1[k] + summ[k]) / nslt[k]
sum2 = 0.
for i in range(len(mus[k])): #loop over processors
for j in range(len(
mus[k][i])): #loop over samples on processors
if k > 0:
sum2 += ((mus[k][i][j] + musm[k][i][j]) - E[k])**2
else:
sum2 += (mus[k][i][j] - E[k])**2
V[k] = sum2 / nslt[k]
import pdb
pdb.set_trace()
if rank == 0:
self.DVCon.evalFunctions(funcs, includeLinear=True)
self.DVCon2.evalFunctions(funcs, includeLinear=True)
eq0 = funcs['eqs']
sa0 = funcs['sas']
else:
eq0 = None
sa0 = None
eq = comm.bcast(eq0, root=0)
sa = comm.bcast(sa0, root=0)
outputs['Cd_m'] = sum(E)
outputs['Cd_v'] = V[0] #by assumption
rho = self.uoptions['rho']
outputs['Cd_r'] = sum(E) + rho * math.sqrt(V[0])
if self.ooptions['use_area_con']:
outputs['SA'] = sa
else:
outputs['TC'] = funcs['tcs']
outputs['EQ'] = eq
outputs['N1'] = self.N1
#outputs['Cd'] = inputs['a']*inputs['a']
def compute_partials(self, inputs, J):
dvdict = {'pnts': inputs['a']}
funcs = {}
funcSens = {}
nslp = []
nslt = []
for k in range(self.Lmax):
nslp.append(len(self.cases[k][rank]))
nslt.append(sum([len(self.cases[k][x]) for x in range(size)]))
sump = []
musp = []
sum1 = []
sum2 = []
mus = []
sumpm = []
muspm = []
summ = []
musm = []
pmup = []
psump = [] #numpy.zeros(len(inputs['a']))
pmu = []
psum1 = []
pmupm = []
psumpm = [] #numpy.zeros(len(inputs['a']))
pmum = []
psumm = []
E = numpy.zeros(self.Lmax)
V = numpy.zeros(self.Lmax)
#import pdb; pdb.set_trace()
for k in range(self.Lmax):
sump.append(0.0)
musp.append(numpy.zeros(nslp[k]))
sumpm.append(0.)
muspm.append(numpy.zeros(nslp[k]))
pmup.append([])
psump.append(numpy.zeros(len(inputs['a'])))
pmupm.append([])
psumpm.append(numpy.zeros(len(inputs['a'])))
for i in range(nslp[k]):
saconstsm = self.samplep[k][i].tolist()
self.saconsts = saconstsm + self.saconstsb
self.solvers[k][i].setOption('SAConsts', self.saconsts)
self.solvers[k][i].DVGeo.setDesignVars(dvdict)
self.aps[k][i].setDesignVars(dvdict)
self.solvers[k][i](self.aps[k][i])
self.solvers[k][i].evalFunctions(self.aps[k][i], funcs)
self.solvers[k][i].evalFunctionsSens(self.aps[k][i], funcSens,
['cd'])
astr = self.gridSol + "_" + str(self.cases[k][rank][i]) + "_cd"
arr = [x * (1. / nslt[k]) for x in funcSens[astr]['pnts']]
musp[k][i] = funcs[astr]
sump[k] += funcs[astr]
pmup[k].append(arr[0])
psump[k] += arr[0]
if k > 0:
self.solvers[k][i + nslp[k]].setOption(
'SAConsts', self.saconsts)
self.solvers[k][i + nslp[k]].DVGeo.setDesignVars(dvdict)
#import pdb; pdb.set_trace()
self.aps[k][i + nslp[k]].setDesignVars(dvdict)
self.solvers[k][i + nslp[k]](self.aps[k][i + nslp[k]])
self.solvers[k][i + nslp[k]].evalFunctions(
self.aps[k][i + nslp[k]], funcs)
self.solvers[k][i + nslp[k]].evalFunctionsSens(
self.aps[k][i + nslp[k]], funcSens, ['cd'])
astr = self.gridSol + "_" + str(
self.cases[k][rank][i]) + "_m_cd"
arr = [x * (1. / nslt[k]) for x in funcSens[astr]['pnts']]
muspm[k][i] = -funcs[astr]
sumpm[k] += -funcs[astr]
pmupm[k].append(-arr[0])
psumpm[k] -= arr[0]
# compute mean and variance
psum2 = numpy.zeros(len(inputs['a']))
for k in range(self.Lmax):
sum1.append(comm.allreduce(sump[k]))
mus.append(comm.allgather(musp[k]))
summ.append(comm.allreduce(sumpm[k]))
musm.append(comm.allgather(muspm[k]))
psum1.append(comm.allreduce(psump[k]))
pmu.append(comm.allgather(pmup[k]))
psumm.append(comm.allreduce(psumpm[k]))
pmum.append(comm.allgather(pmupm[k]))
E[k] = (sum1[k] + summ[k]) / nslt[k]
sum2 = 0.
for i in range(len(mus[0])): #loop over processors
for j in range(len(mus[0][i])): #loop over samples on processors
#import pdb; pdb.set_trace()
sum2 += (mus[0][i][j] - E[0])**2
temp = pmu[0][i][j] * nslt[0] - psum1[0]
arr2 = [x * 2 * (mus[0][i][j] - E[0]) / nslt[0] for x in temp]
psum2 += arr2
V = sum2 / nslt[0]
# compute variance sensitivity
#import pdb; pdb.set_trace()
if rank == 0:
self.DVCon.evalFunctionsSens(funcSens, includeLinear=True)
self.DVCon2.evalFunctionsSens(funcSens, includeLinear=True)
eq0p = funcSens['eqs']['pnts']
sa0p = funcSens['sas']['pnts']
else:
eq0p = None
sa0p = None
eqp = comm.bcast(eq0p, root=0)
sap = comm.bcast(sa0p, root=0)
J['Cd_m', 'a'] = sum(psum1) + sum(psumm)
J['Cd_v', 'a'] = psum2
rho = self.uoptions['rho']
J['Cd_r',
'a'] = sum(psum1) + sum(psumm) + rho * (1. /
(2 * math.sqrt(V))) * psum2
#import pdb; pdb.set_trace()
if self.ooptions['use_area_con']:
J['SA', 'a'] = sap
else:
J['TC', 'a'] = funcSens['tcs']['pnts']
J['EQ', 'a'] = eqp
#J['Cd','a'][0] = 2*inputs['a']
def MLMC(self):
# Use an MLMC algorithm to determine an optimal sample distribution between existing mesh levels
# We do this once before optimization, then compute statistics with the same set of samples at every iteration
# start with initial samples
# Get a set of UQ sample points (LHS), enough for each level at the start
#sys.stdout = open(os.devnull, "w")
# flow characteristics
alpha = 0.0
mach = self.ooptions['mach'] #0.95
Re = self.ooptions['Re'] #50000
Re_L = 1.0
tempR = 540
arearef = 2.0
chordref = 1.0
a_init = self.DVGeo.getValues()
a_init['pnts'][:] = self.ooptions['DVInit']
self.current_samples = self.NS0 * self.Lmax
if rank == 0:
rank0sam = plate_sa_lhs.genLHS(s=self.current_samples)
else:
rank0sam = None
self.sample = comm.bcast(rank0sam, root=0)
# Scatter samples on each level, multi-point parallelism
for i in range(self.Lmax):
self.cases.append(divide_cases(self.NS0, size))
for j in range(len(self.cases[i])):
for k in range(len(self.cases[i][j])):
self.cases[i][j][k] += i * self.NS0
#self.nsp.append(len(self.cases[i][rank]))#int(ns/size) # samples per processor
self.samplep.append(self.sample[self.cases[i][rank]])
#import pdb; pdb.set_trace()
#self.samplep = self.sample[self.cases[rank]]#self.sample[(rank*self.nsp):(rank*self.nsp+(self.nsp))] #shouldn't really need to "scatter" per se
#import pdb; pdb.set_trace()
# for i in range(self.Lmax):
# assert len(self.samplep[i]) == self.nsp[i]
# Actually create solvers (and aeroproblems?) (and mesh?) now
nslp = []
nslt = []
for k in range(self.Lmax):
alist = []
slist = []
mlist = []
alist2 = []
slist2 = []
mlist2 = []
nslp.append(len(self.cases[k][rank]))
nslt.append(sum([len(self.cases[k][x]) for x in range(size)]))
for i in range(nslp[k]):
namestr = self.gridSol + "_" + str(self.cases[k][rank][i])
# create meshes
leveloptions = self.woptions
leveloptions['gridFile'] = self.meshnames[k]
mlist.append(USMesh(options=leveloptions, comm=MPI.COMM_SELF))
# create aeroproblems
aloptions = self.aoptions
aloptions['gridFile'] = self.meshnames[k]
alist.append(
AeroProblem(name=namestr,
alpha=alpha,
mach=mach,
reynolds=Re,
reynoldsLength=Re_L,
T=tempR,
areaRef=arearef,
chordRef=chordref,
evalFuncs=['cd']))
time.sleep(0.1) # this solves a few problems for some reason
# create solvers
slist.append(ADFLOW(options=aloptions, comm=MPI.COMM_SELF))
# if not self.ooptions['run_once']:
# saconstsm = self.samplep[i].tolist()
# else:
saconstsm = self.samplep[k][i].tolist()
self.saconsts = saconstsm + self.saconstsb
slist[i].setOption('SAConsts', self.saconsts)
slist[i].setDVGeo(self.DVGeo)
slist[i].setMesh(mlist[i])
coords = slist[i].getSurfaceCoordinates(
groupName=slist[i].allWallsGroup)
slist[i].DVGeo.addPointSet(coords, 'coords')
if k > 0: #create additional solvers at higher levels for the estimators
# create meshes
namestr = self.gridSol + "_" + str(
self.cases[k][rank][i]) + "_m"
leveloptions = self.woptions
leveloptions['gridFile'] = self.meshnames[k - 1]
mlist2.append(
USMesh(options=leveloptions, comm=MPI.COMM_SELF))
# create aeroproblems
aloptions = self.aoptions
aloptions['gridFile'] = self.meshnames[k - 1]
alist2.append(
AeroProblem(name=namestr,
alpha=alpha,
mach=mach,
reynolds=Re,
reynoldsLength=Re_L,
T=tempR,
areaRef=arearef,
chordRef=chordref,
evalFuncs=['cd']))
time.sleep(
0.1) # this solves a few problems for some reason
# create solvers
slist2.append(ADFLOW(options=aloptions,
comm=MPI.COMM_SELF))
slist2[i].setOption('SAConsts', self.saconsts)
slist2[i].setDVGeo(self.DVGeo)
slist2[i].setMesh(mlist2[i])
coords = slist[i].getSurfaceCoordinates(
groupName=slist2[i].allWallsGroup)
slist2[i].DVGeo.addPointSet(coords, 'coords')
self.aps.append(alist)
self.solvers.append(slist)
self.meshes.append(mlist)
if k > 0:
self.aps[k] += alist2
self.solvers[k] += slist2
self.meshes[k] += mlist2
#import pdb; pdb.set_trace()
# start looping over mesh levels
L = 0
M = 4.0 #0.5 #refinement factor?
converged = 0
eps = self.uoptions['vartol']
sum1 = []
mus = []
sump = []
musp = []
sumpm = []
muspm = []
summ = []
musm = []
E = []
V = []
N1 = []
while ~converged & L < self.Lmax:
# compute start up samples to estimate variance
dvdict = {'pnts': a_init['pnts']}
funcs = {}
nslp = []
nslt = []
for k in range(self.Lmax):
nslp.append(len(self.cases[k][rank]))
nslt.append(sum([len(self.cases[k][x]) for x in range(size)]))
sump.append(0.)
musp.append(numpy.zeros(nslp[L]))
sumpm.append(0.)
muspm.append(numpy.zeros(nslp[L]))
for i in range(nslp[L]):
# just do this again in case
saconstsm = self.samplep[L][i].tolist()
self.saconsts = saconstsm + self.saconstsb
self.solvers[L][i].setOption('SAConsts', self.saconsts)
self.solvers[L][i].DVGeo.setDesignVars(dvdict)
self.aps[L][i].setDesignVars(dvdict)
self.solvers[L][i](self.aps[L][i])
self.solvers[L][i].evalFunctions(self.aps[L][i], funcs)
astr = self.gridSol + "_" + str(self.cases[L][rank][i]) + "_cd"
musp[L][i] = funcs[astr]
sump[L] += funcs[astr]
#import pdb; pdb.set_trace()
if L > 0:
self.solvers[L][i + nslp[L]].setOption(
'SAConsts', self.saconsts)
self.solvers[L][i + nslp[L]].DVGeo.setDesignVars(dvdict)
self.aps[L][i + nslp[L]].setDesignVars(dvdict)
self.solvers[L][i + nslp[L]](self.aps[L][i + nslp[L]])
self.solvers[L][i + nslp[L]].evalFunctions(
self.aps[L][i + nslp[L]], funcs)
astr = self.gridSol + "_" + str(
self.cases[L][rank][i]) + "_m_cd"
muspm[L][i] = -funcs[astr]
sumpm[L] += -funcs[astr]
# compute mean and variance estimate from start up samples
sum1.append(comm.allreduce(sump[L]))
mus.append(comm.allgather(musp[L]))
summ.append(comm.allreduce(sumpm[L]))
musm.append(comm.allgather(muspm[L]))
#import pdb; pdb.set_trace()
# mean at each level
E = numpy.zeros(L + 1)
for l in range(L + 1):
E[l] = (sum1[l] + summ[l]) / nslt[l]
# variance at each level
V = numpy.zeros(L + 1)
for l in range(L + 1):
sum2 = 0.
for i in range(len(mus[l])): #range(size):
for j in range(len(mus[l][i])): #range(self.nsp):
if l > 0:
sum2 += ((mus[l][i][j] + musm[l][i][j]) - E[l])**2
else:
sum2 += (mus[l][i][j] - E[l])**2
V[l] = sum2 / nslt[l]
#import pdb; pdb.set_trace()
# now determine the optimal number of samples at each level
N1.append(0.)
worksum = 0
for l in range(L + 1):
worksum += numpy.sqrt(V[l] * (M**l))
for l in range(L + 1):
nlf = 2 * numpy.sqrt(V[l] / (M**l)) * worksum / (eps * eps)
nlfm = max(nslt[l], math.ceil(nlf))
N1[l] = nlfm
# now compute and generate additional samples at each level
# first partition samples NEVERMIND (just do it once at each level, no need to repeat)
# create the extra number of solvers at each (the current) level
# need to loop everything from here on
for l in range(L + 1):
alist = self.aps[l][0:nslp[l]]
slist = self.solvers[l][0:nslp[l]]
mlist = self.meshes[l][0:nslp[l]]
if l > 0:
alist2 = self.aps[l][nslp[l]:]
slist2 = self.solvers[l][nslp[l]:]
mlist2 = self.meshes[l][nslp[l]:]
self.naddedtot[l] = N1[l] - nslt[l]
self.current_samples += self.naddedtot[l]
#import pdb; pdb.set_trace()
if rank == 0:
rank0sam = plate_sa_lhs.genLHS(s=self.current_samples)
else:
rank0sam = None
self.sample = comm.bcast(rank0sam, root=0)
if self.naddedtot[l] > 0:
temp = divide_cases(self.naddedtot[l], size)
for i in range(len(temp)):
for j in range(len(temp[i])):
temp[i][j] += self.current_samples - self.naddedtot[
l] #self.Lmax*self.NS0 + sum(self.naddedtot[0:L])
else:
temp = []
if len(temp):
for ns in range(size):
self.cases[l][ns] += temp[ns] #append
nslpnew = len(self.cases[l][rank])
nsltnew = sum([len(self.cases[l][x]) for x in range(size)])
#self.nsp[L] = len(self.cases[L][rank]) #int(ns/size) # samples per processor
self.samplep[l] = self.sample[self.cases[l][rank]]
for i in range(nslp[l],
nslpnew): #need it to be just the extra cases
#import pdb; pdb.set_trace()
namestr = self.gridSol + "_" + str(self.cases[l][rank][i])
# create meshes
leveloptions = self.woptions
leveloptions['gridFile'] = self.meshnames[l]
mlist.append(
USMesh(options=leveloptions, comm=MPI.COMM_SELF))
# create aeroproblems
aloptions = self.aoptions
aloptions['gridFile'] = self.meshnames[l]
alist.append(
AeroProblem(name=namestr,
alpha=alpha,
mach=mach,
reynolds=Re,
reynoldsLength=Re_L,
T=tempR,
areaRef=arearef,
chordRef=chordref,
evalFuncs=['cd']))
time.sleep(
0.1) # this solves a few problems for some reason
# create solvers
slist.append(ADFLOW(options=aloptions, comm=MPI.COMM_SELF))
saconstsm = self.samplep[l][i].tolist()
self.saconsts = saconstsm + self.saconstsb
slist[i].setOption('SAConsts', self.saconsts)
slist[i].setDVGeo(self.DVGeo)
slist[i].setMesh(mlist[i])
coords = slist[i].getSurfaceCoordinates(
groupName=slist[i].allWallsGroup)
slist[i].DVGeo.addPointSet(coords, 'coords')
time.sleep(0.1)
if l > 0: #create additional solvers at higher levels for the estimators
# create meshes
#import pdb; pdb.set_trace()
namestr = self.gridSol + "_" + str(
self.cases[l][rank][i]) + "_m"
leveloptions = self.woptions
leveloptions['gridFile'] = self.meshnames[l - 1]
mlist2.append(
USMesh(options=leveloptions, comm=MPI.COMM_SELF))
# create aeroproblems
aloptions = self.aoptions
aloptions['gridFile'] = self.meshnames[l - 1]
alist2.append(
AeroProblem(name=namestr,
alpha=alpha,
mach=mach,
reynolds=Re,
reynoldsLength=Re_L,
T=tempR,
areaRef=arearef,
chordRef=chordref,
evalFuncs=['cd']))
time.sleep(
0.1) # this solves a few problems for some reason
# create solvers
slist2.append(
ADFLOW(options=aloptions, comm=MPI.COMM_SELF))
slist2[i].setOption('SAConsts', self.saconsts)
slist2[i].setDVGeo(self.DVGeo)
slist2[i].setMesh(mlist2[i])
coords = slist[i].getSurfaceCoordinates(
groupName=slist2[i].allWallsGroup)
slist2[i].DVGeo.addPointSet(coords, 'coords')
nslp[l] = nslpnew
nslt[l] = nsltnew
self.aps[l] = alist
self.solvers[l] = slist
self.meshes[l] = mlist
if l > 0:
self.aps[l] += alist2
self.solvers[l] += slist2
self.meshes[l] += mlist2
# compute remaining samples
sump[l] = 0
sumpm[l] = 0
musp[l] = numpy.zeros(nslp[l])
muspm[l] = numpy.zeros(nslp[l])
for i in range(nslp[l]):
# just do this again in case
saconstsm = self.samplep[l][i].tolist()
self.saconsts = saconstsm + self.saconstsb
self.solvers[l][i].setOption('SAConsts', self.saconsts)
self.solvers[l][i].DVGeo.setDesignVars(dvdict)
self.aps[l][i].setDesignVars(dvdict)
self.solvers[l][i](self.aps[l][i])
self.solvers[l][i].evalFunctions(self.aps[l][i], funcs)
astr = self.gridSol + "_" + str(
self.cases[l][rank][i]) + "_cd"
musp[l][i] = funcs[astr]
sump[l] += funcs[astr]
#import pdb; pdb.set_trace()
if l > 0:
self.solvers[l][i + nslp[l]].setOption(
'SAConsts', self.saconsts)
self.solvers[l][i +
nslp[l]].DVGeo.setDesignVars(dvdict)
self.aps[l][i + nslp[l]].setDesignVars(dvdict)
self.solvers[l][i + nslp[l]](self.aps[l][i + nslp[l]])
self.solvers[l][i + nslp[l]].evalFunctions(
self.aps[l][i + nslp[l]], funcs)
astr = self.gridSol + "_" + str(
self.cases[l][rank][i]) + "_m_cd"
muspm[l][i] = -funcs[astr]
sumpm[l] += -funcs[astr]
# compute mean and variance estimate from all samples
sum1[l] = comm.allreduce(sump[l])
mus[l] = comm.allgather(musp[l])
summ[l] = comm.allreduce(sumpm[l])
musm[l] = comm.allgather(muspm[l])
# mean at each level
E[l] = (sum1[l] + summ[l]) / nslt[l]
# variance at each level
sum2 = 0.
for i in range(len(mus[l])): #range(size):
for j in range(len(mus[l][i])): #range(self.nsp):
if l > 0:
sum2 += ((mus[l][i][j] + musm[l][i][j]) - E[l])**2
else:
sum2 += (mus[l][i][j] - E[l])**2
V[l] = sum2 / nslt[l]
# if L == 1:
# import pdb; pdb.set_trace()
L += 1
#import pdb; pdb.set_trace()
#sys.stdout = sys.__stdout__
if rank == 0:
print("MLMC Completed, Samples per level: ", N1)
self.N1 = N1
#import pdb; pdb.set_trace()
# test for convergence
# don't actually need this, won't ever end early
# range = -1:0
# if L > 1 & M**L >= 4:
# con = M**(range.*suml(2,L+1+range)./suml(1,L+1+range))
# converged = (max(abs(con)) < (M-1)*eps/sqrt(2))
# once done, we have aps, solvers, meshes, which is all we need
def dist_samples(self):
# If we already have the number of samples, just create as many solvers as needed at each level
# Just do this after running MLMC() anyway
# flow characteristics
alpha = 0.0
mach = self.ooptions['mach'] #0.95
Re = self.ooptions['Re'] #50000
Re_L = 1.0
tempR = 540
arearef = 2.0
chordref = 1.0
a_init = self.DVGeo.getValues()
a_init['pnts'][:] = self.ooptions['DVInit']
self.current_samples = sum(self.N1)
if rank == 0:
rank0sam = plate_sa_lhs.genLHS(s=self.current_samples)
else:
rank0sam = None
self.sample = comm.bcast(rank0sam, root=0)
#import pdb; pdb.set_trace()
# Scatter samples on each level, multi-point parallelism
self.cases = []
self.samplep = []
for i in range(self.Lmax):
self.cases.append(divide_cases(self.N1[i], size))
for j in range(len(self.cases[i])):
for k in range(len(self.cases[i][j])):
self.cases[i][j][k] += sum(self.N1[0:i])
#self.nsp.append(len(self.cases[i][rank]))#int(ns/size) # samples per processor
self.samplep.append(self.sample[self.cases[i][rank]])
# Actually create solvers (and aeroproblems?) (and mesh?) now
self.aps = []
self.solvers = []
self.meshes = []
nslp = []
nslt = []
for k in range(self.Lmax):
alist = []
slist = []
mlist = []
alist2 = []
slist2 = []
mlist2 = []
nslp.append(len(self.cases[k][rank]))
nslt.append(sum([len(self.cases[k][x]) for x in range(size)]))
for i in range(nslp[k]):
namestr = self.gridSol + "_" + str(self.cases[k][rank][i])
# create meshes
leveloptions = self.woptions
leveloptions['gridFile'] = self.meshnames[k]
mlist.append(USMesh(options=leveloptions, comm=MPI.COMM_SELF))
# create aeroproblems
aloptions = self.aoptions
aloptions['gridFile'] = self.meshnames[k]
alist.append(
AeroProblem(name=namestr,
alpha=alpha,
mach=mach,
reynolds=Re,
reynoldsLength=Re_L,
T=tempR,
areaRef=arearef,
chordRef=chordref,
evalFuncs=['cd']))
time.sleep(0.1) # this solves a few problems for some reason
# create solvers
slist.append(ADFLOW(options=aloptions, comm=MPI.COMM_SELF))
# if not self.ooptions['run_once']:
# saconstsm = self.samplep[i].tolist()
# else:
saconstsm = self.samplep[k][i].tolist()
self.saconsts = saconstsm + self.saconstsb
slist[i].setOption('SAConsts', self.saconsts)
slist[i].setDVGeo(self.DVGeo)
slist[i].setMesh(mlist[i])
coords = slist[i].getSurfaceCoordinates(
groupName=slist[i].allWallsGroup)
slist[i].DVGeo.addPointSet(coords, 'coords')
if k > 0: #create additional solvers at higher levels for the estimators
# create meshes
namestr = self.gridSol + "_" + str(
self.cases[k][rank][i]) + "_m"
leveloptions = self.woptions
leveloptions['gridFile'] = self.meshnames[k - 1]
mlist2.append(
USMesh(options=leveloptions, comm=MPI.COMM_SELF))
# create aeroproblems
aloptions = self.aoptions
aloptions['gridFile'] = self.meshnames[k - 1]
alist2.append(
AeroProblem(name=namestr,
alpha=alpha,
mach=mach,
reynolds=Re,
reynoldsLength=Re_L,
T=tempR,
areaRef=arearef,
chordRef=chordref,
evalFuncs=['cd']))
time.sleep(
0.1) # this solves a few problems for some reason
# create solvers
slist2.append(ADFLOW(options=aloptions,
comm=MPI.COMM_SELF))
slist2[i].setOption('SAConsts', self.saconsts)
slist2[i].setDVGeo(self.DVGeo)
slist2[i].setMesh(mlist2[i])
coords = slist[i].getSurfaceCoordinates(
groupName=slist2[i].allWallsGroup)
slist2[i].DVGeo.addPointSet(coords, 'coords')
self.aps.append(alist)
self.solvers.append(slist)
self.meshes.append(mlist)
if k > 0:
self.aps[k] += alist2
self.solvers[k] += slist2
self.meshes[k] += mlist2
upper=0.05,
axis='y',
scale=10)
DVGeo_back.addGeoDVLocal('local_back',
lower=-0.05,
upper=0.05,
axis='y',
scale=10)
# Add DVGeo object to CFD solver
CFDSolver.setDVGeo(DVGeo_GLOBAL)
#rst dvs
DVCon = DVConstraints(name='con')
DVCon.setDVGeo(DVGeo_GLOBAL)
# Only ADflow has the getTriangulatedSurface Function
DVCon.setSurface(CFDSolver.getTriangulatedMeshSurface())
# Volume constraints
# For the front wing
leList_front = [[0.01, 0, 0.001], [0.01, 0, 0.639]]
teList_front = [[0.239, 0, 0.001], [0.239, 0, 0.639]]
DVCon.addVolumeConstraint(leList_front, teList_front, 20, 20, lower=1.0)
# For the back wing
delta_x = 1.
delta_y = 0.5
class OM_DVGEOCOMP(om.ExplicitComponent):
def initialize(self):
self.options.declare("ffd_file", default=None)
self.options.declare("vsp_file", default=None)
self.options.declare("vsp_options", default=None)
def setup(self):
# create the DVGeo object that does the computations
if self.options["ffd_file"] is not None:
# we are doing an FFD-based DVGeo
ffd_file = self.options["ffd_file"]
self.DVGeo = DVGeometry(ffd_file)
if self.options["vsp_file"] is not None:
# we are doing a VSP based DVGeo
vsp_file = self.options["vsp_file"]
vsp_options = self.options["vsp_options"]
self.DVGeo = DVGeometryVSP(vsp_file, comm=self.comm, **vsp_options)
self.DVCon = DVConstraints()
self.DVCon.setDVGeo(self.DVGeo)
self.omPtSetList = []
def compute(self, inputs, outputs):
# check for inputs thathave been added but the points have not been added to dvgeo
for var in inputs.keys():
# check that the input name matches the convention for points
if var[:2] == "x_":
# trim the _in and add a "0" to signify that these are initial conditions initial
var_out = var[:-3] + "0"
if var_out not in self.omPtSetList:
self.nom_addPointSet(inputs[var],
var_out,
add_output=False)
# inputs are the geometric design variables
self.DVGeo.setDesignVars(inputs)
# ouputs are the coordinates of the pointsets we have
for ptName in self.DVGeo.points:
if ptName in self.omPtSetList:
# update this pointset and write it as output
outputs[ptName] = self.DVGeo.update(ptName).flatten()
# compute the DVCon constraint values
constraintfunc = dict()
self.DVCon.evalFunctions(constraintfunc, includeLinear=True)
comm = self.comm
if comm.rank == 0:
for constraintname in constraintfunc:
outputs[constraintname] = constraintfunc[constraintname]
# we ran a compute so the inputs changed. update the dvcon jac
# next time the jacvec product routine is called
self.update_jac = True
def nom_add_discipline_coords(self, discipline, points=None):
# TODO remove one of these methods to keep only one method to add pointsets
if points is None:
# no pointset info is provided, just do a generic i/o. We will add these points during the first compute
self.add_input("x_%s_in" % discipline,
distributed=True,
shape_by_conn=True)
self.add_output("x_%s0" % discipline,
distributed=True,
copy_shape="x_%s_in" % discipline)
else:
# we are provided with points. we can do the full initialization now
self.nom_addPointSet(points,
"x_%s0" % discipline,
add_output=False)
self.add_input("x_%s_in" % discipline,
distributed=True,
val=points.flatten())
self.add_output("x_%s0" % discipline,
distributed=True,
val=points.flatten())
def nom_addPointSet(self, points, ptName, add_output=True, **kwargs):
# add the points to the dvgeo object
self.DVGeo.addPointSet(points.reshape(len(points) // 3, 3), ptName,
**kwargs)
self.omPtSetList.append(ptName)
if add_output:
# add an output to the om component
self.add_output(ptName, distributed=True, val=points.flatten())
def nom_add_point_dict(self, point_dict):
# add every pointset in the dict, and set the ptset name as the key
for k, v in point_dict.items():
self.nom_addPointSet(v, k)
def nom_addGeoDVGlobal(self, dvName, value, func):
# define the input
self.add_input(dvName, distributed=False, shape=len(value))
# call the dvgeo object and add this dv
self.DVGeo.addGeoDVGlobal(dvName, value, func)
def nom_addGeoDVLocal(self, dvName, axis="y", pointSelect=None):
nVal = self.DVGeo.addGeoDVLocal(dvName,
axis=axis,
pointSelect=pointSelect)
self.add_input(dvName, distributed=False, shape=nVal)
return nVal
def nom_addVSPVariable(self, component, group, parm, **kwargs):
# actually add the DV to VSP
self.DVGeo.addVariable(component, group, parm, **kwargs)
# full name of this DV
dvName = "%s:%s:%s" % (component, group, parm)
# get the value
val = self.DVGeo.DVs[dvName].value.copy()
# add the input with the correct value, VSP DVs always have a size of 1
self.add_input(dvName, distributed=False, shape=1, val=val)
def nom_addThicknessConstraints2D(self,
name,
leList,
teList,
nSpan=10,
nChord=10):
self.DVCon.addThicknessConstraints2D(leList,
teList,
nSpan,
nChord,
lower=1.0,
name=name)
comm = self.comm
if comm.rank == 0:
self.add_output(name,
distributed=True,
val=np.ones((nSpan * nChord, )),
shape=nSpan * nChord)
else:
self.add_output(name, distributed=True, shape=(0, ))
def nom_addThicknessConstraints1D(self, name, ptList, nCon, axis):
self.DVCon.addThicknessConstraints1D(ptList, nCon, axis, name=name)
comm = self.comm
if comm.rank == 0:
self.add_output(name,
distributed=True,
val=np.ones(nCon),
shape=nCon)
else:
self.add_output(name, distributed=True, shape=(0))
def nom_addVolumeConstraint(self,
name,
leList,
teList,
nSpan=10,
nChord=10):
self.DVCon.addVolumeConstraint(leList,
teList,
nSpan=nSpan,
nChord=nChord,
name=name)
comm = self.comm
if comm.rank == 0:
self.add_output(name, distributed=True, val=1.0)
else:
self.add_output(name, distributed=True, shape=0)
def nom_add_LETEConstraint(self, name, volID, faceID, topID=None):
self.DVCon.addLeTeConstraints(volID, faceID, name=name, topID=topID)
# how many are there?
conobj = self.DVCon.linearCon[name]
nCon = len(conobj.indSetA)
comm = self.comm
if comm.rank == 0:
self.add_output(name,
distributed=True,
val=np.zeros((nCon, )),
shape=nCon)
else:
self.add_output(name, distributed=True, shape=0)
return nCon
def nom_addLERadiusConstraints(self, name, leList, nSpan, axis, chordDir):
self.DVCon.addLERadiusConstraints(leList=leList,
nSpan=nSpan,
axis=axis,
chordDir=chordDir,
name=name)
comm = self.comm
if comm.rank == 0:
self.add_output(name,
distributed=True,
val=np.ones(nSpan),
shape=nSpan)
else:
self.add_output(name, distributed=True, shape=0)
def nom_addCurvatureConstraint1D(self, name, start, end, nPts, axis,
**kwargs):
self.DVCon.addCurvatureConstraint1D(start=start,
end=end,
nPts=nPts,
axis=axis,
name=name,
**kwargs)
comm = self.comm
if comm.rank == 0:
self.add_output(name, distributed=True, val=1.0)
else:
self.add_output(name, distributed=True, shape=0)
def nom_addLinearConstraintsShape(self, name, indSetA, indSetB, factorA,
factorB):
self.DVCon.addLinearConstraintsShape(indSetA=indSetA,
indSetB=indSetB,
factorA=factorA,
factorB=factorB,
name=name)
lSize = len(indSetA)
comm = self.comm
if comm.rank == 0:
self.add_output(name,
distributed=True,
val=np.zeros(lSize),
shape=lSize)
else:
self.add_output(name, distributed=True, shape=0)
def nom_addRefAxis(self, **kwargs):
# we just pass this through
return self.DVGeo.addRefAxis(**kwargs)
def nom_setConstraintSurface(self, surface):
# constraint needs a triangulated reference surface at initialization
self.DVCon.setSurface(surface)
def compute_jacvec_product(self, inputs, d_inputs, d_outputs, mode):
# only do the computations when we have more than zero entries in d_inputs in the reverse mode
ni = len(list(d_inputs.keys()))
if mode == "rev" and ni > 0:
# this flag will be set to True after every compute call.
# if it is true, we assume the design has changed so we re-run the sensitivity update
# there can be hundreds of calls to this routine due to thickness constraints,
# as a result, we only run the actual sensitivity comp once and save the jacobians
# this might be better suited with the matrix-based API
if self.update_jac:
self.constraintfuncsens = dict()
self.DVCon.evalFunctionsSens(self.constraintfuncsens,
includeLinear=True)
# set the flag to False so we dont run the update again if this is called w/o a compute in between
self.update_jac = False
for constraintname in self.constraintfuncsens:
for dvname in self.constraintfuncsens[constraintname]:
if dvname in d_inputs:
dcdx = self.constraintfuncsens[constraintname][dvname]
if self.comm.rank == 0:
dout = d_outputs[constraintname]
jvtmp = np.dot(np.transpose(dcdx), dout)
else:
jvtmp = 0.0
d_inputs[dvname] += jvtmp
# OM does the reduction itself
# d_inputs[dvname] += self.comm.reduce(jvtmp, op=MPI.SUM, root=0)
for ptSetName in self.DVGeo.ptSetNames:
if ptSetName in self.omPtSetList:
dout = d_outputs[ptSetName].reshape(
len(d_outputs[ptSetName]) // 3, 3)
# only do the calc. if d_output is not zero on ANY proc
local_all_zeros = np.all(dout == 0)
global_all_zeros = np.zeros(1, dtype=bool)
# we need to communicate for this check otherwise we may hang
self.comm.Allreduce([local_all_zeros, MPI.BOOL],
[global_all_zeros, MPI.BOOL], MPI.LAND)
# global_all_zeros is a numpy array of size 1
if not global_all_zeros[0]:
# TODO totalSensitivityTransProd is broken. does not work with zero surface nodes on a proc
# xdot = self.DVGeo.totalSensitivityTransProd(dout, ptSetName)
xdot = self.DVGeo.totalSensitivity(dout, ptSetName)
# loop over dvs and accumulate
xdotg = {}
for k in xdot:
# check if this dv is present
if k in d_inputs:
# do the allreduce
# TODO reove the allreduce when this is fixed in openmdao
# reduce the result ourselves for now. ideally, openmdao will do the reduction itself when this is fixed. this is because the bcast is also done by openmdao (pyoptsparse, but regardless, it is not done here, so reduce should also not be done here)
xdotg[k] = self.comm.allreduce(xdot[k],
op=MPI.SUM)
# accumulate in the dict
# TODO
# because we only do one point set at a time, we always want the 0th
# entry of this array since dvgeo always behaves like we are passing
# in multiple objective seeds with totalSensitivity. we can remove the [0]
# once we move back to totalSensitivityTransProd
d_inputs[k] += xdotg[k][0]
class PlateComponentMFMC(om.ExplicitComponent):
"""Robust Bump Flow Problem, with LHS Multi Level Monte Carlo Samples"""
def initialize(self):
# Need to modify this dictionary when we change the SA constants
#import pdb; pdb.set_trace()
#sys.stdout = open(os.devnull, "w")
self.aoptions = aeroOptions
self.woptions = warpOptions
self.ooptions = optOptions
self.uoptions = uqOptions
self.Pr = 0.
# Generate FFD and DVs
if rank == 0:
rank0dvg = pf.createFFD()
else:
rank0dvg = None
self.DVGeo = comm.bcast(rank0dvg, root=0)
# Get a full list of every mesh name we have, assume they are ordered properly by level
self.meshnames = self.uoptions['gridFileLevels']
self.Lmax = len(self.meshnames) #as many levels as we have meshes
self.mord = [*range(self.Lmax)]
self.mord.reverse()
if self.Lmax < 3:
raise ValueError('Not enough meshes available, ' + self.Lmax +
' < 3')
# Spalart Allmaras model constants, to be changed in UQ (4 for now)
saconstsm = [0.41, 0.1355, 0.622, 0.66666666667]
self.saconstsb = [7.1, 0.3, 2.0, 1.0, 2.0, 1.2, 0.5, 2.0]
self.saconsts = saconstsm + self.saconstsb
self.aoptions['SAConsts'] = self.saconsts
#self.gridSol = f'{meshname}_{saconstsm}_sol'
solname = self.ooptions['prob_name']
self.gridSol = f'{solname}_sol'
self.cases = []
#self.nsp = [] #keep track per level
self.samplep = []
self.naddedtot = []
for i in range(self.Lmax):
self.naddedtot.append(0)
self.aps = []
self.solvers = []
self.meshes = []
self.NS0 = self.uoptions['NS0']
self.current_samples = self.NS0 * self.Lmax
self.N1 = None
self.a1 = None
self.P = self.uoptions['P']
##########
# call distribute samples here?
if not self.uoptions['use-predetermined-samples']:
self.MFMC()
else:
self.N1 = self.uoptions['predet-N1']
self.a1 = self.uoptions['predet-a1']
self.dist_samples()
##########
# Set constraints, should only need one of those solvers, the meshes are all the same
if rank == 0:
self.DVCon = DVConstraints()
self.DVCon2 = DVConstraints()
self.DVCon.setDVGeo(
self.solvers[0][0].DVGeo.getFlattenedChildren()[1])
self.DVCon2.setDVGeo(self.solvers[0][0].DVGeo)
self.DVCon.setSurface(
self.solvers[0][0].getTriangulatedMeshSurface(
groupName='allSurfaces'))
# set extra group for surface area condition
self.DVCon2.setSurface(
self.solvers[0][0].getTriangulatedMeshSurface(), name='wall')
# DV should be same into page (not doing anything right now)
#import pdb; pdb.set_trace()
lIndex = self.solvers[0][0].DVGeo.getFlattenedChildren(
)[1].getLocalIndex(0)
indSetA = []
indSetB = []
nXc = optOptions['NX']
self.NC = math.trunc(
((1.0 - self.ooptions['DVFraction']) * self.ooptions['NX']))
ind = [
int(nXc / 2) - int(self.NC / 2),
int(nXc / 2) + int(self.NC / 2)
]
for i in range(ind[0], ind[1]):
indSetA.append(lIndex[i, 0, 1])
indSetB.append(lIndex[i, 1, 1])
# for i in range(lIndex.shape[0]):
# indSetA.append(lIndex[i, 0, 1])
# indSetB.append(lIndex[i, 1, 1])
self.DVCon.addLinearConstraintsShape(indSetA,
indSetB,
factorA=1.0,
factorB=-1.0,
lower=0,
upper=0,
name='eqs')
# Thickness constraints (one for each active DV)
#import pdb; pdb.set_trace()
# Maximum thickness of the domain, translates to minimum thickness of bump
ub = 1.0 - self.ooptions['DCMinThick']
tcf = self.ooptions['DCThickFrac']
ra = self.ooptions['bumpBounds']
lim = self.ooptions['DCMinArea']
span = numpy.linspace(0, 1, nXc)
xc = span * (ra[1] - ra[0]) + ra[0]
#ind = range(int(nXc/2) - int(self.NC/2), int(nXc/2) + int(self.NC/2)))
ind = [
int(nXc / 2) - int(tcf * self.NC / 2),
int(nXc / 2) + int(tcf * self.NC / 2)
]
ptList = numpy.zeros([2, 3])
ptList[:, 0] = xc[ind]
ptList[:, 1] = 0.5
ptList[:, 2] = 0.5
if self.ooptions['use_area_con']:
self.DVCon2.addSurfaceAreaConstraint(lower=lim,
upper=10.,
name='sas',
surfaceName='wall')
else:
self.DVCon2.addThicknessConstraints1D(ptList,
self.NC, [0, 0, 1],
lower=0.5,
upper=ub,
name='tcs')
dummy = rank
dsum = comm.allgather(dummy)
sys.stdout = sys.__stdout__
def setup(self):
#initialize shape and set deformation points as inputs
a_init = self.DVGeo.getValues()
a_init['pnts'][:] = self.ooptions['DVInit']
# mult = numpy.linspace(1.0,1.5,num=int(0.5*len(a_init['pnts'])))
# mult = numpy.concatenate((mult, mult))
#if self.ooptions['run_once']:
# a_init['pnts'] = self.ooptions['ro_shape']
#a_init['pnts'] = numpy.multiply(mult, a_init['pnts'])
self.add_input('a', a_init['pnts'], desc="Bump Shape Control Points")
#self.add_input('a', 0.2, desc="Bump Shape Control Points")
if self.ooptions['use_area_con']:
self.add_output('SA', 1.0, desc='Surface Area Constraint')
else:
self.add_output('TC',
numpy.zeros(self.NC),
desc='Thickness Constraints')
self.add_output('Cd_m', 0.0, desc="Mean Drag Coefficient")
self.add_output('Cd_v', 0.0, desc="Variance Drag Coefficient")
self.add_output('Cd_r', 0.0, desc="Robust Drag Objective")
self.add_output('EQ',
numpy.zeros(int(len(a_init['pnts']) / 2)),
desc="Control Point Symmetry")
self.add_output('N1', self.N1, desc="MFMC Samples at each level")
self.add_output('a1', self.a1, desc="MFMC Coeffs at each level")
self.add_output('Pr', 0., desc="MFMC Samples at each level")
def setup_partials(self):
self.declare_partials('Cd_m', 'a', method='exact')
self.declare_partials('Cd_v', 'a', method='exact')
self.declare_partials('Cd_r', 'a', method='exact')
if self.ooptions['use_area_con']:
self.declare_partials('SA', 'a', method='exact')
else:
self.declare_partials('TC', 'a', method='exact')
self.declare_partials('EQ', 'a', method='exact')
def compute(self, inputs, outputs):
# run the bump shape model
#import pdb; pdb.set_trace()
dvdict = {'pnts': inputs['a']}
ntot = self.current_samples
nslp = []
nslt = []
for k in range(self.Lmax):
nslp.append(len(self.cases[k][rank]))
nslt.append(sum([len(self.cases[k][x]) for x in range(size)]))
funcs = {}
sump = []
musp = []
sum1 = []
mus = []
sumpm = []
muspm = []
summ = []
musm = []
E = numpy.zeros(self.Lmax)
V = numpy.zeros(self.Lmax)
for k in range(self.Lmax):
sump.append(0.0)
musp.append(numpy.zeros(nslp[k]))
sumpm.append(0.)
if k > 0:
muspm.append(numpy.zeros(nslp[k - 1]))
else:
muspm.append(numpy.zeros(nslp[k])) #not used
for i in range(nslp[k]):
saconstsm = self.samplep[self.Lmax - 1][i].tolist()
self.saconsts = saconstsm + self.saconstsb
self.solvers[k][i].setOption('SAConsts', self.saconsts)
self.solvers[k][i].DVGeo.setDesignVars(dvdict)
self.aps[k][i].setDesignVars(dvdict)
self.solvers[k][i](self.aps[k][i])
self.solvers[k][i].evalFunctions(self.aps[k][i], funcs)
astr = self.gridSol + "_" + str(self.cases[k][rank][i]) + "_cd"
musp[k][i] = funcs[astr]
sump[k] += funcs[astr]
if k > 0 and i < nslp[k - 1]:
muspm[k][i] = -funcs[astr]
sumpm[k] += -funcs[astr]
# compute mean and variance
for k in range(self.Lmax):
sum1.append(comm.allreduce(sump[k]))
mus.append(comm.allgather(musp[k]))
summ.append(comm.allreduce(sumpm[k]))
musm.append(comm.allgather(muspm[k]))
#import pdb; pdb.set_trace()
if k > 0:
E[k] = (sum1[k] / nslt[k] + summ[k] / nslt[k - 1])
else:
E[k] = (sum1[k] / nslt[k])
sum2 = 0.
for i in range(len(mus[k])): #loop over processors
for j in range(len(
mus[k][i])): #loop over samples on processors
if k > 0:
#sum2 = 0
sum2 += (
(mus[k][i][j] - sum1[k] / nslt[k])**2) / nslt[k]
if j < len(mus[k - 1][i]):
sum2 -= ((musm[k][i][j] - summ[k] / nslt[k - 1])**
2) / nslt[k - 1]
else:
sum2 += ((mus[k][i][j] - E[k])**2) / nslt[k]
V[k] = sum2
#import pdb; pdb.set_trace()
if rank == 0:
self.DVCon.evalFunctions(funcs, includeLinear=True)
self.DVCon2.evalFunctions(funcs, includeLinear=True)
eq0 = funcs['eqs']
sa0 = funcs['sas']
else:
eq0 = None
sa0 = None
eq = comm.bcast(eq0, root=0)
sa = comm.bcast(sa0, root=0)
outputs['Cd_m'] = numpy.dot(self.a1, E)
outputs['Cd_v'] = numpy.dot(self.a1, V) #by assumption
rho = self.uoptions['rho']
outputs['Cd_r'] = numpy.dot(self.a1,
E) + rho * math.sqrt(numpy.dot(self.a1, V))
#import pdb; pdb.set_trace()
if self.ooptions['use_area_con']:
outputs['SA'] = sa
else:
outputs['TC'] = funcs['tcs']
outputs['EQ'] = eq
outputs['N1'] = self.N1
outputs['a1'] = self.a1
outputs['Pr'] = self.Pr
#outputs['Cd'] = inputs['a']*inputs['a']
def compute_partials(self, inputs, J):
dvdict = {'pnts': inputs['a']}
funcs = {}
funcSens = {}
nslp = []
nslt = []
for k in range(self.Lmax):
nslp.append(len(self.cases[k][rank]))
nslt.append(sum([len(self.cases[k][x]) for x in range(size)]))
sump = []
musp = []
sum1 = []
sum2 = []
mus = []
sumpm = []
muspm = []
summ = []
musm = []
pmup = []
psump = [] #numpy.zeros(len(inputs['a']))
pmu = []
psum1 = []
pmupm = []
psumpm = [] #numpy.zeros(len(inputs['a']))
pmum = []
psumm = []
E = numpy.zeros(self.Lmax)
V = numpy.zeros(self.Lmax)
#import pdb; pdb.set_trace()
for k in range(self.Lmax):
sump.append(0.0)
musp.append(numpy.zeros(nslp[k]))
sumpm.append(0.)
if k > 0:
muspm.append(numpy.zeros(nslp[k - 1]))
else:
muspm.append(numpy.zeros(nslp[k])) #not used
pmup.append([])
psump.append(numpy.zeros(len(inputs['a'])))
pmupm.append([])
psumpm.append(numpy.zeros(len(inputs['a'])))
for i in range(nslp[k]):
saconstsm = self.samplep[k][i].tolist()
self.saconsts = saconstsm + self.saconstsb
self.solvers[k][i].setOption('SAConsts', self.saconsts)
self.solvers[k][i].DVGeo.setDesignVars(dvdict)
self.aps[k][i].setDesignVars(dvdict)
self.solvers[k][i](self.aps[k][i])
self.solvers[k][i].evalFunctions(self.aps[k][i], funcs)
self.solvers[k][i].evalFunctionsSens(self.aps[k][i], funcSens,
['cd'])
astr = self.gridSol + "_" + str(self.cases[k][rank][i]) + "_cd"
arr = [
x * (self.a1[k] / nslt[k]) for x in funcSens[astr]['pnts']
]
musp[k][i] = funcs[astr]
sump[k] += funcs[astr]
pmup[k].append(arr[0])
psump[k] += arr[0]
if k > 0 and i < nslp[k - 1]:
arrm = [
x * (self.a1[k] / nslt[k - 1])
for x in funcSens[astr]['pnts']
]
muspm[k][i] = -funcs[astr]
sumpm[k] += -funcs[astr]
pmupm[k].append(-arrm[0])
psumpm[k] -= arrm[0]
# compute mean and variance
psum2 = numpy.zeros(len(inputs['a']))
for k in range(self.Lmax):
sum1.append(comm.allreduce(sump[k]))
mus.append(comm.allgather(musp[k]))
summ.append(comm.allreduce(sumpm[k]))
musm.append(comm.allgather(muspm[k]))
psum1.append(comm.allreduce(psump[k]))
pmu.append(comm.allgather(pmup[k]))
psumm.append(comm.allreduce(psumpm[k]))
pmum.append(comm.allgather(pmupm[k]))
if k > 0:
E[k] = (sum1[k] / nslt[k] + summ[k] / nslt[k - 1])
else:
E[k] = (sum1[k] / nslt[k])
sum2 = 0.
for i in range(len(mus[k])): #loop over processors
for j in range(len(
mus[k][i])): #loop over samples on processors
if k > 0:
#sum2 = 0
sum2 += (
(mus[k][i][j] - sum1[k] / nslt[k])**2) / nslt[k]
if j < len(mus[k - 1][i]):
sum2 -= ((musm[k][i][j] - summ[k] / nslt[k - 1])**
2) / nslt[k - 1]
else:
sum2 += ((mus[k][i][j] - E[k])**2) / nslt[k]
V[k] = sum2
# compute variance sensitivity
psum2 = []
for k in range(self.Lmax):
psum2.append(numpy.zeros(len(inputs['a'])))
for i in range(len(mus[0])): #loop over processors
for j in range(len(
mus[0][i])): #loop over samples on processors
if k > 0:
temp = pmu[k][i][j] * nslt[k] - psum1[k]
arr2 = [
x * 2 * (mus[k][i][j] - sum1[k]) / nslt[k]
for x in temp
]
psum2[k] += arr2
if j < len(mus[k - 1][i]):
temp = pmu[k][i][j] * nslt[k - 1] - psum1[k]
arr2 = [
x * 2 *
(musm[k][i][j] - summ[k] / nslt[k - 1]) /
nslt[k - 1] for x in temp
]
psum2[k] -= arr2
else:
temp = pmu[k][i][j] * nslt[k] - psum1[k]
arr2 = [
x * 2 * (mus[k][i][j] - E[k]) / nslt[k]
for x in temp
]
psum2[k] += arr2
#import pdb; pdb.set_trace()
if rank == 0:
self.DVCon.evalFunctionsSens(funcSens, includeLinear=True)
self.DVCon2.evalFunctionsSens(funcSens, includeLinear=True)
eq0p = funcSens['eqs']['pnts']
sa0p = funcSens['sas']['pnts']
else:
eq0p = None
sa0p = None
eqp = comm.bcast(eq0p, root=0)
sap = comm.bcast(sa0p, root=0)
J['Cd_m', 'a'] = sum(psum1) + sum(psumm)
J['Cd_v', 'a'] = sum(psum2)
rho = self.uoptions['rho']
J['Cd_r', 'a'] = sum(psum1) + sum(psumm) + rho * (
1. / (2 * math.sqrt(numpy.dot(self.a1, V)))) * sum(psum2)
if self.ooptions['use_area_con']:
J['SA', 'a'] = sap
else:
J['TC', 'a'] = funcSens['tcs']['pnts']
J['EQ', 'a'] = eqp
#J['Cd','a'][0] = 2*inputs['a']
def MFMC(self):
# Use an MFMC algorithm to determine optimal sample distribution and coefficients among mesh levels
# We do this once before optimization, then compute statistics with the same set of samples and coeffs at every iteration
# start with initial samples
# Get a set of UQ sample points (LHS), enough for each level at the start
#sys.stdout = open(os.devnull, "w")
# flow characteristics
alpha = 0.0
mach = self.ooptions['mach'] #0.95
Re = self.ooptions['Re'] #50000
Re_L = 1.0
tempR = 540
arearef = 2.0
chordref = 1.0
a_init = self.DVGeo.getValues()
a_init['pnts'][:] = self.ooptions['DVInit']
self.current_samples = self.NS0 * self.Lmax
if rank == 0:
rank0sam = plate_sa_lhs.genLHS(s=self.current_samples)
else:
rank0sam = None
self.sample = comm.bcast(rank0sam, root=0)
N1 = []
a1 = numpy.zeros(self.Lmax)
r1 = numpy.zeros(self.Lmax)
# Scatter samples on each level, multi-point parallelism
for i in range(self.Lmax):
self.cases.append(divide_cases(self.NS0, size))
for j in range(len(self.cases[i])):
for k in range(len(self.cases[i][j])):
self.cases[i][j][k] += i * self.NS0
#self.nsp.append(len(self.cases[i][rank]))#int(ns/size) # samples per processor
self.samplep.append(self.sample[self.cases[i][rank]])
#import pdb; pdb.set_trace()
#self.samplep = self.sample[self.cases[rank]]#self.sample[(rank*self.nsp):(rank*self.nsp+(self.nsp))] #shouldn't really need to "scatter" per se
#import pdb; pdb.set_trace()
# for i in range(self.Lmax):
# assert len(self.samplep[i]) == self.nsp[i]
# Create solvers for the preliminary data
nslp = []
nslt = []
for k in range(self.Lmax):
alist = []
slist = []
mlist = []
nslp.append(len(self.cases[k][rank]))
nslt.append(sum([len(self.cases[k][x]) for x in range(size)]))
for i in range(nslp[k]):
namestr = self.gridSol + "_" + str(self.cases[k][rank][i])
# create meshes
leveloptions = self.woptions
leveloptions['gridFile'] = self.meshnames[self.mord[k]]
#import pdb; pdb.set_trace()
mlist.append(USMesh(options=leveloptions, comm=MPI.COMM_SELF))
# create aeroproblems
aloptions = self.aoptions
aloptions['gridFile'] = self.meshnames[self.mord[k]]
alist.append(
AeroProblem(name=namestr,
alpha=alpha,
mach=mach,
reynolds=Re,
reynoldsLength=Re_L,
T=tempR,
areaRef=arearef,
chordRef=chordref,
evalFuncs=['cd']))
time.sleep(0.1) # this solves a few problems for some reason
# create solvers
slist.append(ADFLOW(options=aloptions, comm=MPI.COMM_SELF))
# if not self.ooptions['run_once']:
# saconstsm = self.samplep[i].tolist()
# else:
saconstsm = self.samplep[0][i].tolist()
self.saconsts = saconstsm + self.saconstsb
slist[i].setOption('SAConsts', self.saconsts)
slist[i].setDVGeo(self.DVGeo)
slist[i].setMesh(mlist[i])
coords = slist[i].getSurfaceCoordinates(
groupName=slist[i].allWallsGroup)
slist[i].DVGeo.addPointSet(coords, 'coords')
self.aps.append(alist)
self.solvers.append(slist)
self.meshes.append(mlist)
# Solve the preliminary samples
# start looping over mesh levels
sumt = []
sumtp = []
nslp = []
nslt = []
sum1 = []
mus = []
sump = []
musp = []
sumpm = []
muspm = []
summ = []
musm = []
Et = numpy.zeros(self.Lmax)
E = numpy.zeros(self.Lmax)
V = numpy.zeros(self.Lmax)
S = numpy.zeros(self.Lmax)
N1 = []
for k in range(self.Lmax):
nslp.append(len(self.cases[k][rank]))
nslt.append(sum([len(self.cases[k][x]) for x in range(size)]))
dvdict = {'pnts': a_init['pnts']}
funcs = {}
sumtp.append(0.0)
sump.append(0.)
musp.append(numpy.zeros(nslp[k]))
sumpm.append(0.)
muspm.append(numpy.zeros(nslp[k]))
for i in range(nslp[k]):
# just do this again in case
saconstsm = self.samplep[0][i].tolist()
self.saconsts = saconstsm + self.saconstsb
self.solvers[k][i].setOption('SAConsts', self.saconsts)
self.solvers[k][i].DVGeo.setDesignVars(dvdict)
self.aps[k][i].setDesignVars(dvdict)
pc0 = time.process_time()
self.solvers[k][i](self.aps[k][i])
self.solvers[k][i].evalFunctions(self.aps[k][i], funcs)
pc1 = time.process_time()
astr = self.gridSol + "_" + str(self.cases[k][rank][i]) + "_cd"
musp[k][i] = funcs[astr]
sump[k] += funcs[astr]
sumtp[k] += (pc1 - pc0)
# compute mean and variance estimate from start up samples
for k in range(self.Lmax):
sumt.append(comm.allreduce(sumtp[k]))
sum1.append(comm.allreduce(sump[k]))
mus.append(comm.allgather(musp[k]))
summ.append(comm.allreduce(sumpm[k]))
musm.append(comm.allgather(muspm[k]))
mus[k] = numpy.concatenate(mus[k][:])
musm[k] = numpy.concatenate(musm[k][:])
#import pdb; pdb.set_trace()
# mean at each level
Et[k] = sumt[k] / nslt[k]
E[k] = (sum1[k]) / nslt[k] #+summ[k]
sum2 = 0.
for i in range(len(mus[k])): #loop over processors
sum2 += (mus[k][i] - E[k])**2
V[k] = sum2 / nslt[k]
S[k] = math.sqrt(V[k])
# compute correlation matrix and rearrange models if necessary
ordered = False
while not ordered:
rho = numpy.corrcoef(mus)
ordered = True # check if contradicted
#tarr = rho[0,1:]
for k in range(self.Lmax - 2):
test = rho[0, 1 + k]**2 - rho[0, 2 + k]**2
if test < 0:
ordered = False
tarr = -rho[0, :]**2
if not ordered:
sind = numpy.argsort(tarr)
#import pdb; pdb.set_trace()
self.mord[:] = [self.mord[i] for i in sind]
E[:] = [E[i] for i in sind]
Et[:] = [Et[i] for i in sind]
V[:] = [V[i] for i in sind]
S[:] = [S[i] for i in sind]
mus[:] = [mus[i] for i in sind]
# now compute N1 and a1 using sigma, rho, w, and p
for k in range(self.Lmax):
a1[k] = S[0] * rho[0, k] / S[k]
if k == 0:
r1[k] = 1
elif k == self.Lmax - 1:
work = Et[0] * (rho[0, k]**2)
work /= Et[k] * (1 - rho[0, 1]**2)
r1[k] = math.sqrt(work)
else:
work = Et[0] * (rho[0, k - 1]**2 - rho[0, k]**2)
work /= Et[k] * (1 - rho[0, 1]**2)
r1[k] = math.sqrt(work)
for k in range(self.Lmax):
N1.append(0)
nsf = self.P / numpy.dot(Et, r1)
N1[0] = math.ceil(nsf)
for k in range(self.Lmax):
nsf = N1[0] * r1[k]
N1[k] = math.ceil(nsf)
# limit the number of samples on the last one to pass the sanity check, for debug
sanity = numpy.dot(N1, Et)
if sanity > 1.2 * self.P:
N1n = (self.P - numpy.dot(N1[0:self.Lmax - 2],
Et[0:self.Lmax - 2])) / Et[self.Lmax - 1]
N1[self.Lmax - 1] = math.ceil(N1n)
self.Pr = numpy.dot(N1, Et)
self.N1 = N1
self.a1 = a1
#import pdb; pdb.set_trace()
if rank == 0:
print("MFMC Completed, Samples per level: ", N1)
# call dist_samples after this
def dist_samples(self):
# If we already have the number of samples, just create as many solvers as needed at each level
# Just do this after running MLMC() anyway
# flow characteristics
alpha = 0.0
mach = self.ooptions['mach'] #0.95
Re = self.ooptions['Re'] #50000
Re_L = 1.0
tempR = 540
arearef = 2.0
chordref = 1.0
a_init = self.DVGeo.getValues()
a_init['pnts'][:] = self.ooptions['DVInit']
self.current_samples = sum(self.N1)
if rank == 0:
rank0sam = plate_sa_lhs.genLHS(s=self.current_samples)
else:
rank0sam = None
self.sample = comm.bcast(rank0sam, root=0)
#import pdb; pdb.set_trace()
# Scatter samples on each level, multi-point parallelism
self.cases = []
self.samplep = []
for i in range(self.Lmax):
self.cases.append(divide_cases(self.N1[i], size))
for j in range(len(self.cases[i])):
for k in range(len(self.cases[i][j])):
self.cases[i][j][k] += sum(self.N1[0:i])
#self.nsp.append(len(self.cases[i][rank]))#int(ns/size) # samples per processor
self.samplep.append(self.sample[self.cases[i][rank]])
# Actually create solvers (and aeroproblems?) (and mesh?) now
self.aps = []
self.solvers = []
self.meshes = []
nslp = []
nslt = []
for k in range(self.Lmax):
alist = []
slist = []
mlist = []
nslp.append(len(self.cases[k][rank]))
nslt.append(sum([len(self.cases[k][x]) for x in range(size)]))
for i in range(nslp[k]):
namestr = self.gridSol + "_" + str(self.cases[k][rank][i])
# create meshes
leveloptions = self.woptions
leveloptions['gridFile'] = self.meshnames[self.mord[k]]
mlist.append(USMesh(options=leveloptions, comm=MPI.COMM_SELF))
# create aeroproblems
aloptions = self.aoptions
aloptions['gridFile'] = self.meshnames[self.mord[k]]
alist.append(
AeroProblem(name=namestr,
alpha=alpha,
mach=mach,
reynolds=Re,
reynoldsLength=Re_L,
T=tempR,
areaRef=arearef,
chordRef=chordref,
evalFuncs=['cd']))
time.sleep(0.1) # this solves a few problems for some reason
# create solvers
slist.append(ADFLOW(options=aloptions, comm=MPI.COMM_SELF))
saconstsm = self.samplep[self.Lmax - 1][i].tolist()
self.saconsts = saconstsm + self.saconstsb
slist[i].setOption('SAConsts', self.saconsts)
slist[i].setDVGeo(self.DVGeo)
slist[i].setMesh(mlist[i])
coords = slist[i].getSurfaceCoordinates(
groupName=slist[i].allWallsGroup)
slist[i].DVGeo.addPointSet(coords, 'coords')
self.aps.append(alist)
self.solvers.append(slist)
self.meshes.append(mlist)
func=twist,
lower=-10,
upper=10,
scale=0.01)
# Set up local design variables
DVGeo.addLocalDV("local", lower=-0.5, upper=0.5, axis="y", scale=1)
# Add DVGeo object to CFD solver
CFDSolver.setDVGeo(DVGeo)
# rst dvgeo (end)
# ======================================================================
# DVConstraint Setup, and Thickness and Volume Constraints
# ======================================================================
# rst dvconVolThick (beg)
DVCon = DVConstraints()
DVCon.setDVGeo(DVGeo)
# Only ADflow has the getTriangulatedSurface Function
DVCon.setSurface(CFDSolver.getTriangulatedMeshSurface())
# Volume constraints
leList = [[0.01, 0, 0.001], [7.51, 0, 13.99]]
teList = [[4.99, 0, 0.001], [8.99, 0, 13.99]]
DVCon.addVolumeConstraint(leList,
teList,
nSpan=20,
nChord=20,
lower=1.0,
scaled=True)
class PlateComponent(om.ExplicitComponent):
"""Deterministic Bump Flow Problem"""
def initialize(self):
# Need to modify this dictionary when we change the SA constants
sys.stdout = open(os.devnull, "w")
self.aoptions = aeroOptions
self.woptions = warpOptions
self.ooptions = optOptions
# Generate FFD and DVs
self.DVGeo = pf.createFFD()
# starting flat mesh
meshname = self.aoptions['gridFile']
gridFile = meshname
# flow characteristics
alpha = 0.0
mach = self.ooptions['mach']#0.95
Re = self.ooptions['Re']#50000
Re_L = 1.0
temp = 540
arearef = 2.0
chordref = 1.0
# Spalart Allmaras model constants, to be changed in UQ
saconstsm = [0.41, 0.1355, 0.622, 0.66666666667, 7.1, 0.3, 2.0]
self.saconsts = saconstsm + [1.0, 2.0, 1.2, 0.5, 2.0]
self.aoptions['SAConsts'] = self.saconsts
#self.gridSol = f'{meshname}_{saconstsm}_sol'
solname = self.ooptions['prob_name']
self.gridSol = f'{solname}_sol'
# Aerodynamic problem description
self.ap = AeroProblem(name=self.gridSol, alpha=alpha, mach=mach, reynolds=Re, reynoldsLength=Re_L, T=temp, areaRef=arearef, chordRef=chordref,
evalFuncs=['cd'])
# Create solver
self.CFDSolver = ADFLOW(options=self.aoptions, comm=MPI.COMM_WORLD)
self.CFDSolver.setDVGeo(self.DVGeo)
# Set up mesh warping
self.mesh = USMesh(options=self.woptions, comm=MPI.COMM_WORLD)
self.CFDSolver.setMesh(self.mesh)
# Try setting the DVGeo coordinates here
coords = self.CFDSolver.getSurfaceCoordinates(groupName=self.CFDSolver.allWallsGroup)
self.CFDSolver.DVGeo.addPointSet(coords, 'coords')
self.CFDSolver.DVGeo.getFlattenedChildren()[1].writePlot3d("ffdp_opt_def.xyz")
# Set constraints
self.DVCon = DVConstraints()
self.DVCon2 = DVConstraints()
self.DVCon.setDVGeo(self.CFDSolver.DVGeo.getFlattenedChildren()[1])
self.DVCon2.setDVGeo(self.CFDSolver.DVGeo)
self.DVCon.setSurface(self.CFDSolver.getTriangulatedMeshSurface(groupName='allSurfaces'))
# set extra group for surface area condition
self.DVCon2.setSurface(self.CFDSolver.getTriangulatedMeshSurface(), name='wall')
# DV should be same into page (not doing anything right now)
#import pdb; pdb.set_trace()
lIndex = self.CFDSolver.DVGeo.getFlattenedChildren()[1].getLocalIndex(0)
indSetA = []
indSetB = []
nXc = optOptions['NX']
self.NC = math.trunc(((1.0 - self.ooptions['DVFraction'])*self.ooptions['NX']))
ind = [int(nXc/2) - int(self.NC/2), int(nXc/2) + int(self.NC/2)]
for i in range(ind[0], ind[1]):
indSetA.append(lIndex[i, 0, 1])
indSetB.append(lIndex[i, 1, 1])
# for i in range(lIndex.shape[0]):
# indSetA.append(lIndex[i, 0, 1])
# indSetB.append(lIndex[i, 1, 1])
self.DVCon.addLinearConstraintsShape(indSetA, indSetB, factorA=1.0, factorB=-1.0, lower=0, upper=0, name='eqs')
# Thickness constraints (one for each active DV)
#import pdb; pdb.set_trace()
# Maximum thickness of the domain, translates to minimum thickness of bump
ub = 1.0 - self.ooptions['DCMinThick']
tcf = self.ooptions['DCThickFrac']
ra = self.ooptions['bumpBounds']
lim = self.ooptions['DCMinArea']
span = numpy.linspace(0, 1, nXc)
xc = span * (ra[1] - ra[0]) + ra[0]
#ind = range(int(nXc/2) - int(self.NC/2), int(nXc/2) + int(self.NC/2)))
ind = [int(nXc/2) - int(tcf*self.NC/2), int(nXc/2) + int(tcf*self.NC/2)]
ptList = numpy.zeros([2, 3])
ptList[:,0] = xc[ind]
ptList[:,1] = 0.5
ptList[:,2] = 0.5
if self.ooptions['use_area_con']:
self.DVCon2.addSurfaceAreaConstraint(lower=lim, upper=10., name='sas', surfaceName='wall')
else:
self.DVCon2.addThicknessConstraints1D(ptList, self.NC, [0,0,1], lower=0.5, upper=ub, name='tcs')
sys.stdout = sys.__stdout__
def setup(self):
#initialize shape and set deformation points as inputs
a_init = self.CFDSolver.DVGeo.getValues()
a_init['pnts'][:] = self.ooptions['DVInit']
# mult = numpy.linspace(1.0,1.5,num=int(0.5*len(a_init['pnts'])))
# mult = numpy.concatenate((mult, mult))
# a_init['pnts'] = numpy.multiply(mult, a_init['pnts'])
#if self.ooptions['run_once']:
# a_init['pnts'] = self.ooptions['ro_shape']
self.add_input('a', a_init['pnts'], desc="Bump Shape Control Points")
#self.add_input('a', 0.2, desc="Bump Shape Control Points")
if self.ooptions['use_area_con']:
self.add_output('SA', 1.0, desc='Surface Area Constraint')
else:
self.add_output('TC', numpy.zeros(self.NC), desc='Thickness Constraints')
self.add_output('Cd', 0.0, desc="Drag Coefficient")
self.add_output('EQ', numpy.zeros(int(len(a_init['pnts'])/2)), desc="Control Point Symmetry")
def setup_partials(self):
self.declare_partials('Cd','a', method='exact')
if self.ooptions['use_area_con']:
self.declare_partials('SA','a', method='exact')
else:
self.declare_partials('TC','a', method='exact')
self.declare_partials('EQ','a', method='exact')
def compute(self, inputs, outputs):
# run the bump shape model
# move the mesh
#import pdb; pdb.set_trace()
dvdict = {'pnts':inputs['a']}
self.CFDSolver.DVGeo.setDesignVars(dvdict)
self.ap.setDesignVars(dvdict)
#self.CFDSolver.DVGeo.update("coords")
# Solve and evaluate functions
funcs = {}
self.CFDSolver(self.ap)
self.DVCon.evalFunctions(funcs, includeLinear=True)
self.DVCon2.evalFunctions(funcs, includeLinear=True)
self.CFDSolver.evalFunctions(self.ap, funcs)
str = self.gridSol + '_cd'
outputs['Cd'] = funcs[str]
if self.ooptions['use_area_con']:
outputs['SA'] = funcs['sas']
else:
outputs['TC'] = funcs['tcs']
outputs['EQ'] = funcs['eqs']
#outputs['Cd'] = inputs['a']*inputs['a']
def compute_partials(self, inputs, J):
# move the mesh
#import pdb; pdb.set_trace()
dvdict = {'pnts':inputs['a']}
self.CFDSolver.DVGeo.setDesignVars(dvdict)
self.ap.setDesignVars(dvdict)
#self.CFDSolver.DVGeo.update("coords")
funcSens = {}
#self.CFDSolver(self.ap) #ASSUME WE ALREADY COMPUTED THE SOLUTION
self.DVCon.evalFunctionsSens(funcSens, includeLinear=True)
self.DVCon2.evalFunctionsSens(funcSens, includeLinear=True)
self.CFDSolver.evalFunctionsSens(self.ap, funcSens, ['cd'])
str = self.gridSol + '_cd'
J['Cd','a'] = funcSens[str]['pnts']
if self.ooptions['use_area_con']:
J['SA','a'] = funcSens['sas']['pnts']
else:
J['TC','a'] = funcSens['tcs']['pnts']
J['EQ','a'] = funcSens['eqs']['pnts']
