def ctrls(self):
if self._ctrls is None:
self._ctrls = {}
scta = self.scta
sctb = self.sctb
if self.mirror:
for control in sctb.ctrls:
ctrl = sctb.ctrls[control]
newctrl = ctrl.duplicate(mirror=True)
self._ctrls[control] = newctrl
else:
for control in scta.ctrls:
ctrl = scta.ctrls[control]
newctrl = ctrl.duplicate(mirror=False)
self._ctrls[control] = newctrl
for control in self.ctrls:
ctrl = self._ctrls[control]
if ctrl.uhvec.return_magnitude() == 0.0:
pntal = Vector((ctrl.xhinge - scta.xoc) * scta.chord, 0.0,
-scta.zoc * scta.chord)
pnta = scta.point + scta.crdsys.vector_to_global(pntal)
pntbl = Vector((ctrl.xhinge - sctb.xoc) * sctb.chord, 0.0,
-sctb.zoc * sctb.chord)
pntb = sctb.point + sctb.crdsys.vector_to_global(pntbl)
hvec = pntb - pnta
ctrl.set_hinge_vector(hvec)
return self._ctrls
def vector_to_local(crd: Coordinate, vec: MatrixVector) -> MatrixVector:
"""Transforms a vector from global to this local coordinate system"""
dirx = Vector(crd.dirx.x, crd.dirx.y, crd.dirx.z)
diry = Vector(crd.diry.x, crd.diry.y, crd.diry.z)
dirz = Vector(crd.dirz.x, crd.dirz.y, crd.dirz.z)
x = dirx * vec
y = diry * vec
z = dirz * vec
return MatrixVector(x, y, z)
def angle_between_vectors(veca: Vector, vecb: Vector):
unta = veca.to_unit()
untb = vecb.to_unit()
adb = unta * untb
if adb > 1.0:
adb = 1.0
elif adb < -1.0:
adb = -1.0
return acos(adb)
def trefftz_velocity(self, pnt: Vector):
r = Vector(0.0, pnt.y, pnt.z)
ra = Vector(0.0, self.pnt1.y, self.pnt1.z)
rb = Vector(0.0, self.pnt2.y, self.pnt2.z)
a = r - ra
b = r - rb
axx = Vector(0.0, a.z, -a.y)
bxx = Vector(0.0, b.z, -b.y)
am2 = a * a
bm2 = b * b
vel = (axx / am2 - bxx / bm2) / 2 / pi
return vel
def duplicate(self, mirror=True):
if mirror and self.reverse:
posgain, neggain = -self.neggain, -self.posgain
else:
posgain, neggain = self.posgain, self.neggain
if mirror:
uhvec = Vector(self.uhvec.x, -self.uhvec.y, self.uhvec.z)
else:
uhvec = Vector(self.uhvec.x, self.uhvec.y, self.uhvec.z)
ctrl = PanelControl(self.name, posgain, neggain, self.xhinge)
ctrl.reverse = False
ctrl.set_hinge_vector(uhvec)
return ctrl
def crdsys(self):
if self._crdsys is None:
tilt = radians(self.tilt)
sintilt = sin(tilt)
costilt = cos(tilt)
diry = Vector(0.0, costilt, sintilt)
twist = radians(self.twist)
sintwist = sin(twist)
costwist = cos(twist)
dirx = Vector(costwist, sintwist * sintilt, -sintwist * costilt)
dirz = dirx**diry
self._crdsys = Coordinate(self.point, dirx, diry, dirz)
return self._crdsys
def get_profile(self, offset: bool=True):
num = self.cnum*2+1
profile = zero_matrix_vector((1, num), dtype=float)
for i in range(self.cnum+1):
n = num-i-1
j = n-num
profile[0, i] = Vector(self.airfoil.xl[j], 0.0, self.airfoil.yl[j])
profile[0, n] = Vector(self.airfoil.xu[j], 0.0, self.airfoil.yu[j])
profile.z[absolute(profile.z) < tol] = 0.0
profile.z = profile.z*self.thkcor
if offset:
offvec = Vector(self.xoc, 0.0, self.zoc)
profile = profile-offvec
return profile
def latticesystem_from_dict(sysdct: dict):
from .latticesurface import latticesurface_from_json
from .latticeresult import latticeresult_from_json
from .latticetrim import latticetrim_from_json
from pyvlm.tools import masses_from_json, masses_from_data
from os.path import dirname, join, exists
jsonfilepath = sysdct['source']
path = dirname(jsonfilepath)
for surfdata in sysdct['surfaces']:
for sectdata in surfdata['sections']:
if 'airfoil' in sectdata:
airfoil = sectdata['airfoil']
if airfoil[-4:] == '.dat':
airfoil = join(path, airfoil)
if not exists(airfoil):
print(f'Airfoil {airfoil} does not exist.')
del sectdata['airfoil']
else:
sectdata['airfoil'] = airfoil
name = sysdct['name']
sfcs = []
for surfdata in sysdct['surfaces']:
sfc = latticesurface_from_json(surfdata)
sfcs.append(sfc)
bref = sysdct['bref']
cref = sysdct['cref']
sref = sysdct['sref']
xref = sysdct['xref']
yref = sysdct['yref']
zref = sysdct['zref']
rref = Vector(xref, yref, zref)
lsys = LatticeSystem(name, sfcs, bref, cref, sref, rref)
masses = {}
if 'masses' in sysdct:
if isinstance(sysdct['masses'], list):
masses = masses_from_data(sysdct['masses'])
elif isinstance(sysdct['masses'], str):
if sysdct['masses'][-5:] == '.json':
massfilename = sysdct['masses']
massfilepath = join(path, massfilename)
masses = masses_from_json(massfilepath)
lsys.masses = masses
if 'cases' in sysdct and sysdct:
lsys.mesh()
for i in range(len(sysdct['cases'])):
resdata = sysdct['cases'][i]
if 'trim' in resdata:
latticetrim_from_json(lsys, resdata)
else:
latticeresult_from_json(lsys, resdata)
lsys.source = jsonfilepath
return lsys
def add_section_constraint(self,
sind: int,
ksx: float = 0.0,
ksy: float = 0.0,
ksz: float = 0.0,
gsx: float = 0.0,
gsy: float = 0.0,
gsz: float = 0.0):
self._rbdy = None
for i, strp in enumerate(self.srfc.strps):
inda = 2 * i
if strp.prfa is self.srfc.scts[sind]:
self.pntinds[inda] = len(self.rpnts)
self.rpnts.append(strp.prfa.point)
self.ks.append(Vector(ksx, ksy, ksz))
self.gs.append(Vector(gsx, gsy, gsz))
def vector_from_dict(vectordata):
x, y, z = None, None, None
if 'x' in vectordata:
x = vectordata['x']
if 'y' in vectordata:
y = vectordata['y']
if 'z' in vectordata:
z = vectordata['z']
return Vector(x, y, z)
def __getitem__(self, key):
x = self.x[key]
y = self.y[key]
z = self.z[key]
if isinstance(x, matrix) and isinstance(y, matrix) and isinstance(
z, matrix):
return MatrixVector(x, y, z)
else:
return Vector(x, y, z)
def sum(self, axis=None, dtype=None, out=None):
x = self.x.sum(axis=axis, dtype=dtype, out=out)
y = self.y.sum(axis=axis, dtype=dtype, out=out)
z = self.z.sum(axis=axis, dtype=dtype, out=out)
if isinstance(x, matrix) and isinstance(y, matrix) and isinstance(
z, matrix):
return MatrixVector(x, y, z)
else:
return Vector(x, y, z)
def create_trim_result(self):
from ..classes import LatticeTrim
ltrm = LatticeTrim(self.name, self.sys)
ltrm.set_density(rho=self.density)
ltrm.set_state(speed=self.speed, qco2V=self.qco2V)
ltrm.set_targets(CLt=self.CL)
rcg = Vector(self.mass.xcm, self.mass.ycm, self.mass.zcm)
ltrm.set_cg(rcg)
return ltrm
def __init__(self,
grda: Vector,
grdb: Vector,
diro: Vector,
ind: int = None):
self.grda = grda
self.grdb = grdb
self.diro = diro.to_unit()
self.ind = ind
def baryinv(self):
if self._baryinv is None:
self._baryinv = []
for i in range(self.num):
dirx = self.dirxab[0, i]
diry = self.diryab[0, i]
dirz = self.dirzab[0, i]
grda = self.grdr[0, i-1]
grdb = self.grdr[0, i]
grdal = Vector(grda*dirx, grda*diry, grda*dirz)
grdbl = Vector(grdb*dirx, grdb*diry, grdb*dirz)
amat = zeros((3, 3), dtype=float)
amat[0, :] = 1.0
amat[1, 1] = grdal.x
amat[2, 1] = grdal.y
amat[1, 2] = grdbl.x
amat[2, 2] = grdbl.y
self._baryinv.append(inv(amat))
return self._baryinv
def tolist(self):
lst = []
for i in range(self.shape[0]):
lst.append([])
for j in range(self.shape[1]):
x = self.x[i, j]
y = self.y[i, j]
z = self.z[i, j]
lst[-1].append(Vector(x, y, z))
return lst
def sign_local_z(self, pnts: MatrixVector, betx: float = 1.0):
vecs = pnts - self.pnto
nrm = self.nrm
if betx != 1.0:
vecs.x = vecs.x / betx
nrm = Vector(self.nrm.x / betx, self.nrm.y, self.nrm.z)
locz = vecs * nrm
sgnz = ones(locz.shape, float)
sgnz[locz <= 0.0] = -1.0
return sgnz
def return_mirror(self):
pnt = Vector(self.pnt.x, -self.pnt.y, self.pnt.z)
chord = self.chord
twist = self.twist
sct = LatticeSection(pnt, chord, twist)
sct.camber = self.camber
sct.bspc = self.bspc
sct.yspace = self.yspace
sct.ctrls = self.ctrls
sct.cdo = self.cdo
sct.mirror = True
return sct
def trefftz_plane_velocities(self,
pnts: MatrixVector,
betx: float = 1.0,
bety: float = 1.0,
betz: float = 1.0):
# Trailing Vortex A
agcs = self.relative_mach(pnts,
self.grda,
betx=betx,
bety=bety,
betz=betz)
dirxa = -self.diro
dirza = self.nrm
dirya = dirza**dirxa
alcs = MatrixVector(agcs * dirxa, agcs * dirya, agcs * dirza)
alcs.x = zeros(alcs.shape, dtype=float)
axx = MatrixVector(alcs.x, -alcs.z, alcs.y)
am2 = square(alcs.y) + square(alcs.z)
chkam2 = absolute(am2) < tol
am2r = zeros(pnts.shape, dtype=float)
reciprocal(am2, where=logical_not(chkam2), out=am2r)
faca = -1.0
veldl = elementwise_multiply(axx, am2r) * faca
veldl.x[chkam2] = 0.0
veldl.y[chkam2] = 0.0
veldl.z[chkam2] = 0.0
dirxi = Vector(dirxa.x, dirya.x, dirza.x)
diryi = Vector(dirxa.y, dirya.y, dirza.y)
dirzi = Vector(dirxa.z, dirya.z, dirza.z)
velda = MatrixVector(veldl * dirxi, veldl * diryi,
veldl * dirzi) * faca
# Trailing Vortex B
bgcs = self.relative_mach(pnts,
self.grdb,
betx=betx,
bety=bety,
betz=betz)
dirxb = self.diro
dirzb = self.nrm
diryb = dirzb**dirxb
blcs = MatrixVector(bgcs * dirxb, bgcs * diryb, bgcs * dirzb)
blcs.x = zeros(blcs.shape, dtype=float)
bxx = MatrixVector(blcs.x, -blcs.z, blcs.y)
bm2 = square(blcs.y) + square(blcs.z)
chkbm2 = absolute(bm2) < tol
bm2r = zeros(pnts.shape, dtype=float)
reciprocal(bm2, where=logical_not(chkbm2), out=bm2r)
facb = 1.0
veldl = elementwise_multiply(bxx, bm2r) * facb
veldl.x[chkbm2] = 0.0
veldl.y[chkbm2] = 0.0
veldl.z[chkbm2] = 0.0
dirxi = Vector(dirxb.x, diryb.x, dirzb.x)
diryi = Vector(dirxb.y, diryb.y, dirzb.y)
dirzi = Vector(dirxb.z, diryb.z, dirzb.z)
veldb = MatrixVector(veldl * dirxi, veldl * diryi,
veldl * dirzi) * facb
# Add Together
veld = velda + veldb
return veld / twoPi
def panelsystem_from_geom(sysdct: Dict[str, any]):
if 'source' in sysdct:
path = dirname(sysdct['source'])
for surfdata in sysdct['surfaces']:
for sectdata in surfdata['sections']:
if 'airfoil' in sectdata:
airfoil = sectdata['airfoil']
if airfoil is not None:
if airfoil[-4:] == '.dat':
airfoil = join(path, airfoil)
if not exists(airfoil):
print(f'Airfoil {airfoil} does not exist.')
del sectdata['airfoil']
else:
sectdata['airfoil'] = airfoil
srfcs = []
for surfdata in sysdct['surfaces']:
srfcs.append(panelsurface_from_json(surfdata))
name = sysdct['name']
bref = sysdct['bref']
cref = sysdct['cref']
sref = sysdct['sref']
xref = sysdct['xref']
yref = sysdct['yref']
zref = sysdct['zref']
rref = Vector(xref, yref, zref)
psys = PanelSystem(name, bref, cref, sref, rref)
psys.set_geom(srfcs)
masses = {}
if 'masses' in sysdct:
if isinstance(sysdct['masses'], list):
masses = masses_from_json(sysdct['masses'])
elif isinstance(sysdct['masses'], str):
if sysdct['masses'][-5:] == '.json':
massfilename = sysdct['masses']
massfilepath = join(path, massfilename)
masses = masses_from_json(massfilepath)
psys.masses = masses
if 'cases' in sysdct and sysdct:
panelresults_from_dict(psys, sysdct['cases'])
if 'source' in sysdct:
psys.source = sysdct['source']
return psys
def update(self):
self.bfrc = (self.bspc[1] - self.bspc[0]) / (self.bspc[2] -
self.bspc[0])
self.pnls = []
self.leni = self.pnt2 - self.pnt1
self.pnti = self.pnt1 + self.bfrc * self.leni
self.lent = Vector(0.0, self.leni.y, self.leni.z)
self.dyt = self.leni.y
self.dzt = self.leni.z
self.dst = (self.dyt**2 + self.dzt**2)**0.5
pnta = self.pnt1 + 0.25 * self.crd1 * ihat
pntb = self.pnt2 + 0.25 * self.crd2 * ihat
vecab = pntb - pnta
self.pntq = pnta + self.bfrc * vecab
def panelsection_from_json(sectdata: dict) -> PanelSection:
xpos = sectdata['xpos']
ypos = sectdata['ypos']
zpos = sectdata['zpos']
point = Vector(xpos, ypos, zpos)
chord = sectdata['chord']
airfoilstr = sectdata['airfoil']
if airfoilstr is not None:
if airfoilstr[-4:] == '.dat':
airfoil = airfoil_from_dat(airfoilstr)
elif airfoilstr[0:4].upper() == 'NACA':
code = airfoilstr[4:].strip()
if len(code) == 4:
airfoil = NACA4(code)
else:
raise ValueError(f'Airfoil identified by {airfoilstr:s} does not exist.')
else:
airfoil = None
twist = 0.0
if 'twist' in sectdata:
twist = sectdata['twist']
sect = PanelSection(point, chord, twist, airfoil)
if 'bnum' in sectdata:
sect.bnum = sectdata['bnum']
if 'bspc' in sectdata:
sect.bspc = sectdata['bspc']
if 'tilt' in sectdata:
sect.set_tilt(sectdata['tilt'])
if 'xoc' in sectdata:
sect.xoc = sectdata['xoc']
if 'zoc' in sectdata:
sect.zoc = sectdata['zoc']
if 'noload' in sectdata:
sect.noload = sectdata['noload']
if 'nohsv' in sectdata:
sect.nohsv = sectdata['nohsv']
if 'nomesh' in sectdata:
sect.nomesh = sectdata['nomesh']
if sect.nomesh:
sect.noload = True
# sect.nohsv = True
if 'controls' in sectdata:
for name in sectdata['controls']:
ctrl = panelcontrol_from_dict(name, sectdata['controls'][name])
sect.add_control(ctrl)
return sect
def update(self):
strpres = self.pres.strpres
self.frctot = Vector(0.0, 0.0, 0.0)
self.momtot = Vector(0.0, 0.0, 0.0)
for i, strp in enumerate(self.strc.strps):
ind = strp.ind
rrel = strp.point - self.rref
self.frctot += strpres.stfrc[ind, 0]
self.momtot += strpres.stmom[ind, 0] + rrel**strpres.stfrc[ind, 0]
self.rfrc, self.rmom = self.strc.rbdy.return_reactions(self.frctot, self.momtot)
self.ptfrc = zero_matrix_vector(self.strc.pnts.shape, dtype=float)
self.ptmom = zero_matrix_vector(self.strc.pnts.shape, dtype=float)
ptfrcb = Vector(0.0, 0.0, 0.0)
ptmomb = Vector(0.0, 0.0, 0.0)
for i, strp in enumerate(self.strc.strps):
ind = strp.ind
inda = 2*i
indb = inda + 1
ptfrca = ptfrcb
ptmoma = ptmomb
if inda in self.strc.pntinds:
ptfrca -= self.rfrc[self.strc.pntinds[inda]]
ptmoma -= self.rmom[self.strc.pntinds[inda]]
ptfrcb = ptfrca - strpres.stfrc[ind, 0]
ptmomb = ptmoma - strpres.stmom[ind, 0]
rrel = strp.point - self.strc.pnts[indb, 0]
ptmomb -= rrel**strpres.stfrc[ind, 0]
rrel = self.strc.pnts[indb, 0]-self.strc.pnts[inda, 0]
ptmomb -= rrel**ptfrca
self.ptfrc[inda, 0] = ptfrca
self.ptfrc[indb, 0] = ptfrcb
self.ptmom[inda, 0] = ptmoma
self.ptmom[indb, 0] = ptmomb
fx = self.ptfrc.x.transpose().tolist()[0]
fy = self.ptfrc.y.transpose().tolist()[0]
fz = self.ptfrc.z.transpose().tolist()[0]
mx = self.ptmom.x.transpose().tolist()[0]
my = self.ptmom.y.transpose().tolist()[0]
mz = self.ptmom.z.transpose().tolist()[0]
self.frcmin = Vector(min(fx), min(fy), min(fz))
self.frcmax = Vector(max(fx), max(fy), max(fz))
self.mommin = Vector(min(mx), min(my), min(mz))
self.mommax = Vector(max(mx), max(my), max(mz))
def panelcontrol_from_dict(name: str, controldata: dict):
xhinge = controldata['xhinge']
posgain = 1.0
if 'posgain' in controldata:
posgain = controldata['posgain']
neggain = 1.0
if 'neggain' in controldata:
neggain = controldata['neggain']
ctrl = PanelControl(name, posgain, neggain, xhinge)
hvec = Vector(0.0, 0.0, 0.0)
if 'hvec' in controldata:
hvec = vector_from_dict(controldata['hvec'])
ctrl.set_hinge_vector(hvec)
reverse = False
if 'reverse' in controldata:
reverse = controldata['reverse']
ctrl.reverse = reverse
return ctrl
def latticesection_from_json(sectdata: dict):
if 'xpos' in sectdata:
xpos = sectdata['xpos']
else:
raise ValueError()
if 'ypos' in sectdata:
ypos = sectdata['ypos']
else:
raise ValueError()
if 'zpos' in sectdata:
zpos = sectdata['zpos']
else:
raise ValueError()
point = Vector(xpos, ypos, zpos)
if 'chord' in sectdata:
chord = sectdata['chord']
else:
raise ValueError()
if 'twist' in sectdata:
twist = sectdata['twist']
else:
twist = 0.0
sct = LatticeSection(point, chord, twist)
if 'cdo' in sectdata:
sct.set_cdo(sectdata['cdo'])
if 'noload' in sectdata:
sct.set_noload(sectdata['noload'])
if 'airfoil' in sectdata:
sct.set_airfoil(sectdata['airfoil'])
if 'bnum' in sectdata and 'bspc' in sectdata:
bnum = sectdata['bnum']
bspc = sectdata['bspc']
if bspc == 'equal':
sct.set_span_equal_spacing(bnum)
elif bspc in ('full-cosine', 'cosine'):
sct.set_span_cosine_spacing(bnum)
elif bspc == 'semi-cosine':
sct.set_span_semi_cosine_spacing(bnum)
if 'controls' in sectdata:
for name in sectdata['controls']:
ctrl = latticecontrol_from_json(name, sectdata['controls'][name])
sct.add_control(ctrl)
return sct
def point_res(self, pnlres: matrix, pnt: Vector, ttol: float = 0.1):
vecg = pnt - self.pnto
gres = self.grid_res(pnlres)
pres = pnlres[self.ind, 0]
r = 0.0
for i in range(self.num):
dirx = self.dirxab[0, i]
diry = self.diryab[0, i]
dirz = self.dirzab[0, i]
vecl = Vector(vecg * dirx, vecg * diry, vecg * dirz)
ainv = self.baryinv[i]
bmat = matrix([[1.0], [vecl.x], [vecl.y]])
tmat = ainv * bmat
to, ta, tb = tmat[0, 0], tmat[1, 0], tmat[2, 0]
mint = min(to, ta, tb)
if mint > -ttol:
ro, ra, rb = pres, gres[i - 1], gres[i]
r = ro * to + ra * ta + rb * tb
break
return r
def mirror_section_in_y(self, ymir: float=0.0):
point = Vector(self.point.x, ymir-self.point.y, self.point.z)
chord = self.chord
twist = self.twist
airfoil = self.airfoil
sect = PanelSection(point, chord, twist, airfoil)
sect.mirror = True
sect.bnum = self.bnum
sect.bspc = self.bspc
sect.nomesh = self.nomesh
sect.noload = self.noload
sect.nohsv = self.nohsv
sect.xoc = self.xoc
sect.zoc = self.zoc
sect.bval = self.bval
sect.bpos = -self.bpos
sect.ctrls = self.ctrls
if self.tilt is not None:
sect.set_tilt(-self._tilt)
return sect
def velocity(self, pnt: Vector):
r = pnt
ra = self.pnta
rb = self.pntb
a = r - ra
b = r - rb
am = a.return_magnitude()
bm = b.return_magnitude()
vel = Vector(0.0, 0.0, 0.0)
if pnt != self.pnti:
axb = a**b
if axb.return_magnitude() != 0.0:
den = am * bm + a * b
vel += axb / den * (1 / am + 1 / bm)
axx = Vector(0.0, a.z, -a.y)
if axx.return_magnitude() != 0.0:
den = am - a.x
vel += axx / den / am
bxx = Vector(0.0, b.z, -b.y)
if bxx.return_magnitude() != 0.0:
den = bm - b.x
vel -= bxx / den / bm
vel = vel / fourPi
return vel
def panelsurface_from_json(surfdata: dict, display: bool=False):
name = surfdata['name']
if 'mirror' in surfdata:
mirror = surfdata['mirror']
else:
mirror = False
if 'cnum' in surfdata:
cnum = surfdata['cnum']
if display: print(f'Loading Surface: {name:s}')
# Read Section Variables
sects = []
for sectdata in surfdata['sections']:
sect = panelsection_from_json(sectdata)
sects.append(sect)
if sect.airfoil is not None:
sect.airfoil.update(cnum)
# Linear Interpolate Missing Variables
x, y, z, c, a, af = [], [], [], [], [], []
for sect in sects:
x.append(sect.point.x)
y.append(sect.point.y)
z.append(sect.point.z)
c.append(sect.chord)
a.append(sect.twist)
af.append(sect.airfoil)
if None in y and None in z:
raise ValueError('Need at least ypos or zpos specified in sections.')
elif None in y:
y = linear_interpolate_none(z, y)
elif None in z:
z = linear_interpolate_none(y, z)
lensects = len(sects)
b = [0.0]
for i in range(lensects-1):
bi = b[i]+sqrt((y[i+1]-y[i])**2+(z[i+1]-z[i])**2)
b.append(bi)
x = linear_interpolate_none(b, x)
c = linear_interpolate_none(b, c)
a = linear_interpolate_none(b, a)
af = linear_interpolate_airfoil(b, af)
for i, sect in enumerate(sects):
sect.point.x = x[i]
sect.point.y = y[i]
sect.point.z = z[i]
sect.chord = c[i]
sect.twist = a[i]
sect.airfoil = af[i]
# Read in Function Data
funcs = {}
if 'functions' in surfdata:
for funcdata in surfdata['functions']:
func = panelfunction_from_json(funcdata)
funcs[func.var] = func
# Entire Surface Position
xpos, ypos, zpos = 0.0, 0.0, 0.0
if 'xpos' in surfdata:
xpos = surfdata['xpos']
if 'ypos' in surfdata:
ypos = surfdata['ypos']
if 'zpos' in surfdata:
zpos = surfdata['zpos']
point = Vector(xpos, ypos, zpos)
twist = 0.0
if 'twist' in surfdata:
twist = surfdata['twist']
if 'ruled' in surfdata:
ruled = surfdata['ruled']
else:
ruled = False
for sect in sects:
sect.offset_position(xpos, ypos, zpos)
sect.offset_twist(twist)
sect.ruled = ruled
close = True
if 'close' in surfdata:
close = surfdata['close']
surf = PanelSurface(name, point, twist, mirror, sects, funcs, close)
surf.set_chord_spacing(cnum)
return surf
#%%
# Import Dependencies
from time import perf_counter
from pygeom.geom3d import Vector
from pygeom.matrix3d import zero_matrix_vector
from pyapm.classes.poly import Poly
from pyapm.classes.horseshoe import HorseShoe
from pyapm.tools.functions import mean, derivative
from matplotlib.pyplot import figure
from numpy.matlib import absolute
#%%
# Create Trailing Edge Vortex
grda = Vector(-0.25, 0.75, 0.0)
grdb = Vector(-1.25, -1.25, 0.0)
diro = Vector(1.0, 0.25, 0.0).to_unit()
hsv = HorseShoe(grda, grdb, diro)
grds = [
grdb,
grdb + 100*diro,
grda + 100*diro,
grda
]
poly = Poly(grds)
#%%
# Mesh Points
xorg = 0.0
