def main(): #\
"""Function to Instantiate a JacketSE Assembly: \n
INPUTS \n
All hardwired, so edit the quantities below all the way to the line "#________________ DO NOT MODIFY THE FOLLOWING ________________#" \n
-See JacketOpt_PyOPT for more information. \n
OUTPUTS \n
myjckt -jacket assembly instance \n\n
Optimization parameters: \n\n
f0 -float, target frequency [Hz]
f0epsilon -float, f0*(1+f0epsilon) will not be exceeded \n
jcktDTRmin -Float, minimum jacket member DTR allowed, mostly for 60+waterdepths. \n
mxftprint -Float, max allowed foot print [m]
guesses -Float(n), guesses for all design variables check out DesVar class. \n
bounds -Float(n,2), bounds for all design variables check out DesVar class. \n\n
SAMPLE CALLS: \n
1.OPTIMIZATION: python JacketOpt_ExtCobyla.py C:\RRD\PYTHON\WISDEM\JacketSE\src\jacketse\MyJacketInputs.py \n
2.OPTIMIZATION: python JacketOpt_PyOPT.py C:\RRD\PYTHON\WISDEM\JacketSE\src\jacketse\MyJacketInputs.py True \n
3.BUILD JACKET: python >>> myjacket=C:\RRD\PYTHON\WISDEM\JacketSE\src\jacketse\MyJacketInputs.py \n
"""
#Set inputs ###----ALL USER INPUT----###
Jcktins = JcktGeoInputs()
Jcktins.nlegs = 4
Jcktins.nbays = 4 #CJB To change this you must change tleg, below
Jcktins.batter = 30.5495 #=(-43.127+24.614)/(5.939-5.333)
#Jcktins.dck_botz =15.651
Jcktins.dck_botz = 16.51 #CJBe
Jcktins.dck_width = 8. + 1.2
Jcktins.weld2D = 0.
Jcktins.VPFlag = True #vertical pile T/F; to enable piles in frame3DD set pileinputs.ndiv>0
Jcktins.clamped = True #whether or not the bottom of the structure is rigidly connected. Use False when equivalent spring constants are being used.
Jcktins.AFflag = False #whether or not to use apparent fixity piles
Jcktins.PreBuildTPLvl = 0 #if >0, the TP is prebuilt according to rules per PreBuildTP
#______________________________________________#
#Soil inputs
Soilinputs = SoilGeoInputs()
Soilinputs.zbots = -np.array([3., 5., 7., 15., 30., 50.])
Soilinputs.gammas = np.array(
[10000., 10000., 10000., 10000., 10000., 10000.])
Soilinputs.cus = np.array([60000., 60000., 60000., 60000., 60000., 60000.])
Soilinputs.phis = np.array(
[26., 26., 26., 26., 26., 26]
) #np.array([36.,33.,26.,37.,35.,37.5])#np.array([36.,33.,26.,37.,35.,37.5])
Soilinputs.delta = 25.
Soilinputs.sndflg = True
Soilinputs.PenderSwtch = False #True
Soilinputs.SoilSF = 1.
#______________________________________________#
#Water and wind inputs
#Water and wind inputs
Waterinputs = WaterInputs() #CJBtest Max thrust case
Waterinputs.wdepth = 50. #CJBtest Max thrust case
Waterinputs.wlevel = 50. #CJBtest Max thrust case #Distance from bottom of structure to surface THIS, I believe is no longer needed as piles may be negative in z, to check and remove in case
Waterinputs.T = 12. #CJBtest Max thrust case #Wave Period
Waterinputs.HW = 10 #CJBtest Max thrust case #Wave Height
Waterinputs.Cd = 3. #CJBtest Max thrust case #Drag Coefficient, enhanced to account for marine growth and other members not calculated
Waterinputs.Cm = 8. #2. #CJBtest Max thrust case #Added mass Coefficient
#WaterInputs.Uc=0.0 #CJBtest Max thrust case test
Windinputs = WindInputs() #CJBtest Max thrust case
Windinputs.HH = 87.6 + .51 + Jcktins.dck_botz + 4 #CJBtest Max thrust case (4 comes from the height of the TP) #CHECK HOW THIS COMPLIES....
Windinputs.Cdj = 4. #CJBtest Max thrust case #Drag Coefficient for jacket members, enhanced to account for TP drag not calculated otherwise
Windinputs.Cdt = 2 #CJBtest Max thrust case #Drag Coefficient for tower, enhanced to account for TP drag not calculated otherwise
Windinputs.al_shear = .2 #CJBtest Max thrust case test
Windinputs.U50HH = 20 #CJBtest Max thrust case test #assumed gust speed
#Windinputs.U50HH=70. #CJBtest Max wind speed case test #assumed gust speed
#______________________________________________#
#Pile data
Pilematin = MatInputs()
Pilematin.matname = np.array(['steel'
]) #CJB Changed this from RC into steel
Pilematin.E = np.array([2.1e11])
Pilematin.G = np.array([8.07690e+10])
Pilematin.rho = np.array(
[3339.12]
) * 34274.82 / 36876. #From Test04.txt in SD, to check with official FAST certtest
Pileinputs = PileGeoInputs()
Pileinputs.Pilematins = Pilematin
Pileinputs.ndiv = 0 #CJB Change this from 1 to 0 #3 ###----USER INPUT----###
Pileinputs.Dpile = 2.082
Pileinputs.tpile = 0.491
Pileinputs.Lp = 0. #[m] Embedment length
#______________________________________________#
#Legs data
legmatin = MatInputs()
legmatin.matname = (['steel'])
legmatin.rho = np.array([7850.])
Dleg = np.asarray([1.2]).repeat(Jcktins.nbays +
1) #e.g., np.array([2.0,1.8,1.6,1.6,1.6])
tleg = np.asarray([0.05, 0.05, 0.035, 0.035,
0.035]) #CJB Length must be 1 more than (nbays)
leginputs = LegGeoInputs()
leginputs.legZbot = 4.5 ###----USER INPUT----###
leginputs.ndiv = 1 ###----USER INPUT----###
leginputs.legmatins = legmatin
leginputs.Dleg = Dleg
leginputs.tleg = tleg
#The following is a passthrough variables
legbot_stmphin = (
45.5 - 43.127
) #=2.373 Distance from bottom of leg to second joint along z; must be>0
#______________________________________________#
#Xbrc data
Xbrcmatin = MatInputs()
Xbrcmatin.matname = np.array(['steel']).repeat(Jcktins.nbays)
Xbrcmatin.rho = np.array([7850.])
Dbrc = np.asarray([0.8]).repeat(Jcktins.nbays)
tbrc = np.asarray([0.02]).repeat(Jcktins.nbays)
Xbrcinputs = XBrcGeoInputs()
Xbrcinputs.Dbrc = Dbrc
Xbrcinputs.tbrc = tbrc
Xbrcinputs.ndiv = 1 ###----USER INPUT----###
Xbrcinputs.Xbrcmatins = Xbrcmatin
Xbrcinputs.precalc = False #This can be set to true if we want Xbraces to be precalculated in D and t, in which case the above set Dbrc and tbrc would be overwritten
#______________________________________________#
#Mbrc data
Mbrcmatin = MatInputs()
Mbrcmatin.matname = np.array(['steel'])
Mbrcmatin.rho = np.array([7850.])
Mbrcinputs = MudBrcGeoInputs()
Mbrcinputs.Dbrc_mud = 0.8 ###----USER INPUT----###
Mbrcinputs.tbrc_mud = 0.02
Mbrcinputs.ndiv = 2 ###----USER INPUT----###
Mbrcinputs.Mbrcmatins = Mbrcmatin
Mbrcinputs.precalc = False #This can be set to true if we want Mudbrace to be precalculated in D and t, in which case the above set Dbrc_mud and tbrc_mud would be overwritten
#______________________________________________#
#Hbrc data
Hbrcmatin = MatInputs()
Hbrcmatin.matname = np.array(['steel'])
Hbrcmatin.rho = np.array([7850.])
Dbrc_hbrc = 1.1 ###----USER INPUT----###
Hbrcinputs = HBrcGeoInputs()
Hbrcinputs.Dbrch = Dbrc_hbrc ###----USER INPUT----###
Hbrcinputs.ndiv = 0
Hbrcinputs.Hbrcmatins = Hbrcmatin
Hbrcinputs.precalc = True #This can be set to true if we want Hbrace to be set=Xbrace top D and t, in which case the above set Dbrch and tbrch would be overwritten
#______________________________________________#
#TP data
#Note PrebuildTPLvl is set in JacketIns ###----USER INPUT----###
#TP lumped mass data
TPlumpinputs = TPlumpMass() ###----ALL USER INPUT----###
TPlumpinputs.mass = 666.e3 #-98385.33+( 7850.*4*np.pi/4.*(1.2**2-(1.2-2.*0.04)**2)*4) #[kg] TO MODIFY AFTER WE ASSESS OVERALL TP MASS, to be reduced for the steel weight
TPlumpinputs.CMoff = np.array([
0., 0., 2.
]) #CG of concrete block is 2 m above intersection of diagonal braces
TPlumpinputs.I = 1. / 12 * TPlumpinputs.mass * np.array(
[8.**2 + 4.**2, 8.**2 + 4.**2, 8.**2 + 8.**2, 0., 0., 0.])
TPstrtmatin = MatInputs()
TPstmpsmatin = MatInputs()
TPgirdmatin = MatInputs()
TPbrcmatin = MatInputs()
TPstemmatin = MatInputs()
TPstmpsmatin.matname = np.array(['steel'])
TPstmpsmatin.rho = np.array([7850.])
TPstrtmatin.matname = np.array(['steel'])
TPstrtmatin.rho = np.array([1350.])
TPbrcmatin.matname = np.array(['steel'])
TPbrcmatin.rho = np.array(
[1350.]
) #np.array([7850.]) tpstrucmass=np.pi/4*(1.2**2-(1.2-2*0.04)**2)*7850*4*4 7850.*tpstrucmass/myjckt.TP.TPouts.mass=1462.185
TPgirdmatin.matname = np.array(['steel'])
TPgirdmatin.rho = np.array([1350.])
TPstemmatin.matname = np.array(['steel'
]).repeat(2) ###----ALL USER INPUT----###
TPstemmatin.rho = np.array([1350.])
TPinputs = TPGeoInputs()
TPinputs.TPstrtmatins = TPstrtmatin
TPinputs.TPbrcmatins = TPbrcmatin
TPinputs.TPstemmatins = TPstemmatin
TPinputs.TPstmpmatins = TPstmpsmatin
TPinputs.TPgirdmatins = TPgirdmatin
#Set TP dimensions as leg and brace dimensions
TPinputs.Dstrut = 1.2 ###----ALL USER INPUT----###
TPinputs.tstrut = 0.04
TPinputs.Dgir = TPinputs.Dstrut
TPinputs.tgir = TPinputs.tstrut
TPinputs.Dbrc = TPinputs.Dstrut
TPinputs.tbrc = TPinputs.tstrut
###----ALL USER INPUT----###
TPinputs.hstump = 0.499 #(16.15-15.651)
TPinputs.Dstump = 1.2
TPinputs.tstump = 0.04
TPinputs.stumpndiv = 1
TPinputs.brcndiv = 1
TPinputs.girndiv = 1
TPinputs.strutndiv = 1
TPinputs.stemndiv = 1
TPinputs.nstems = 3
TPinputs.Dstem = np.array([5.6]).repeat(TPinputs.nstems)
TPinputs.tstem = np.array([0.032, 0.032, 0.032])
TPinputs.hstem = np.array([(4.) / TPinputs.nstems]).repeat(TPinputs.nstems)
#______________________________________________#
#Tower data
Twrmatin = MatInputs()
Twrmatin.matname = np.array(['heavysteel']) #CJBtest
Twrmatin.rho = np.array([8500.]) #CJBtest
#Twrmatin.matname=np.array(['steel'])
#Twrmatin.rho=np.array([7850.])
Twrinputs = TwrGeoInputs()
Twrinputs.Twrmatins = Twrmatin
#Twrinputs.Htwr=88.15 #Trumped by HH
Twrinputs.Htwr2frac = 1. / 87.6 #CJBtest #fraction of tower height with constant x-section
Twrinputs.ndiv = np.array([
1, 1
]) #ndiv for uniform and tapered section ###----USER INPUT----###
Twrinputs.DeltaZmax = 5. #[m], maximum FE element length allowed in the tower members (i.e. the uniform and the tapered members)
Twrinputs.Db = 6. #CJBtest
Twrinputs.DTRb = Twrinputs.Db / (1.3 * .027) #CJBtest
Twrinputs.Dt = 3.87 #CJBtest
Twrinputs.DTRt = Twrinputs.Dt / (1.3 * .019) #CJBtest
#Set whether or not DTRb and DTRt for the tower are the same. Note if next set to False it will trump DTRt setting above
Twrinputs.DTRsdiff = True ##SET THIS TO TRUE IF YOU WANT DTRs to be different between base and top
#If you use the following 12 lines, The geometry defined above is ignored
#CJBtest Don't use stations
#ztwr=np.array([20.15,21.15,32.15,42.15,54.15,64.15,74.15,83.15,88.15]) -20.15
#Dtwr=np.array([5.6,5.577,5.318,5.082,4.8,4.565,4.329,4.118,4])
#ttwr=np.array([0.032,0.032,0.03,0.028,0.024,0.022,0.02,0.03,0.03])
#pmtwr=np.array([ np.array([20.15,54.15,88.15])-20.15,[1.9e3,1.4e3,1.0e3]]).T #(3,2) first col z's, second weights
#Interpolate data to refine tower discretization
#dz=1. #[m] maximum deltaz allowed in discretization
#ztwr2=np.linspace(ztwr[0],ztwr[-1],round((ztwr[-1]-ztwr[0])/dz)) #New discretization
#Dtwr_interp=interp1d(ztwr,Dtwr)
#ttwr_interp=interp1d(ztwr,ttwr)
#Twrinputs.ztwr=ztwr2
#Twrinputs.Dtwr=Dtwr_interp(ztwr2)
#Twrinputs.ttwr=ttwr_interp(ztwr2)
#Twrinputs.TwrlumpedMass=np.zeros([pmtwr.shape[0],11])
#Twrinputs.TwrlumpedMass[:,0:2]=pmtwr
TwrRigidTop = False #False=Account for RNA via math rather than a physical rigidmember
#______________________________________________#
#RNA data
RNAins = RNAprops()
RNAins.mass = 350.e3 #CJBtest #[kg]
RNAins.I[0] = 114930678 #CJBtest #[kg m2]
RNAins.I[1] = 22035403 #CJBtest #[kg m2]
RNAins.I[2] = 18759742.50 #CJBtest #[kg m2]
RNAins.I[4] = 503710.47 #CJBtest #[kg m2]
RNAins.CMoff[0] = -1.13 #CJBtest #[m]
RNAins.CMoff[2] = .51 #CJBtest #[m]
#RNAins.Thoff[2]=2.4 #CJBtest #[m]
RNAins.yawangle = 0. #CJBtest #angle with respect to global X, CCW looking from above, wind from left
RNAins.rna_weightM = True
UtilAssembly.tilt = 5.0 #CJBtest test
#______________________________________________#
#RNA loads Fx-z, Mxx-zz
RNA_F = np.array(
[
1284744.196, 0., -112400.5527, 3963732.762, 896380.8464,
-346781.6819
]
) #CJBtest Max thrust case #unfactored thrust, though accounting for gust and dynamic effects (no IEC PSF though)
#RNA_F=np.array([188038.8045,0.,-16451.2637,0.0,131196.8431,0.0]) #CJBtest Max wind speed case #unfactored thrust, though accounting for gust and dynamic effects (no IEC PSF though)
#RNA_F=np.array([1000.e3,0.,0.,0.,0.,0.])
#______________________________________________#
# Frame3DD parameters ###----ALL USER INPUT----###
FrameAuxIns = Frame3DDaux()
FrameAuxIns.sh_fg = 1 #shear flag-->Timoshenko
FrameAuxIns.deltaz = 5.
FrameAuxIns.geo_fg = 0
FrameAuxIns.nModes = 6 # number of desired dynamic modes of vibration
FrameAuxIns.Mmethod = 1 # 1: subspace Jacobi 2: Stodola
FrameAuxIns.lump = 0 # 0: consistent mass ... 1: lumped mass matrix
FrameAuxIns.tol = 1e-9 # mode shape tolerance
FrameAuxIns.shift = 0.0 # shift value ... for unrestrained structures
FrameAuxIns.gvector = np.array([0., 0., -9.8065]) #GRAVITY
#Decide whether or not to consider DLC 6.1 as well
twodlcs = False
#______________________________________________#
#______________________________________________#
# OTHER AUXILIARY CONSTRAINTS AND TARGETS FOR OPTIMIZATION #
#______________________________________________#
#______________________________________________#
#Set Optimization Bounds and guesses for the various variables:
# x= [ batter, Dpile, tpile, Lp, Dleg, tleg, Dbrc, tbrc, Dbrc_mud, tbrc_mud, Dgit, tgir, Db, DTRb Dt, DTRt Htwr2fac dck_widthfact]
MnCnst = np.array([
8., 1., 1. * 0.0254, 20., 1., 1. * 0.0254, 1., 1. * 0.0254, 1.,
1. * 0.0254, 1., 1. * 0.0254, 5., 120., 3., 120., 0.05, 2.
])
MxCnst = np.array([
15., 2.5, 5. * 0.0254, 50., 2.5, 5. * 0.0254, 2., 5. * 0.0254, 2.,
5. * 0.0254, 2., 5. * 0.0254, 7., 200., 4., 200., 0.25, 3.
])
guesses = np.array([
10., 1.5, 1.5 * 0.0254, 26., 1.8, 1.5 * 0.0254, 1.2, 1.5 * 0.0254, 1.2,
1.5 * 0.0254, 1.2, 1.5 * 0.0254, 6., 140., 3.5, 150., 0.2, 2.
])
#SET Maximum Footprint [m]
mxftprint = 30.
#Set target frequency [Hz] and f0epsilon, i.e. fmax=(1+f0eps)*f0
f0 = 0.22
f0epsilon = 0.1
#Set the minminimum DTR allowed for jacket members; mostly for 60+waterdepths
jcktDTRmin = 22.
#_____________________________________________________________#
#________________ DO NOT MODIFY THE FOLLOWING ________________#
#_____________________________________________________________#
bounds = np.vstack((MnCnst, MxCnst))
desvarmeans = np.mean(bounds, 1)
# Now Launch the assembly and pass all of the inputs
#myjckt=set_as_top(JacketSE(Jcktins.clamped,Jcktins.AFflag,twodlcs=twodlcs, wlevel_Ulist=29))#CJB and JQ
myjckt = set_as_top(
JacketSE(Jcktins.clamped, Jcktins.AFflag, twodlcs=twodlcs))
#pySubDyn Parameters CJB+
#SDpySubDynA = pySubDynA()
#INPUTS TO RUN SUBDYN-------------------------------------------------------
#(PATH INFORMATION FOR INPUT FILE AND DRIVER)
Base_name = "5MW_Tower_JEnv_pySubDyn" #Input name here
#INPUT FILE PATH
myjckt.InputFile_name = str(Base_name) + ".txt"
#myjckt.SDpySubDynA.InputFile_name=str(Base_name)+".txt"
myjckt.InputandDriverpath = "C:\wisdem\plugins\JacketSE\src\jacketse\SubDyn\CertTest"
myjckt.InputFile_path = myjckt.InputandDriverpath + os.sep + str(
myjckt.InputFile_name)
#DRIVER PATH
myjckt.Driver_name = str(Base_name) + "D" + ".txt"
myjckt.Driver_path = myjckt.InputandDriverpath + os.sep + str(
myjckt.Driver_name)
myjckt.Driver_path = myjckt.InputandDriverpath + os.sep + str(
myjckt.Driver_name)
#PATH TO RUN SUBDYN
SDEXEpath = "C:\wisdem\plugins\JacketSE\src\jacketse\SubDyn" + os.sep + "bin\SubDyn_Win32.exe"
myjckt.SDpath = str(SDEXEpath) + ' ' + str(myjckt.Driver_path)
#test.SDpath='r'+"'''"+test.SDEXEpath+' '+test.SDDriverpath+"'''"
#PATH TO READ OUTPUT (INPUTS TO READ OUTPUT)
myjckt.Readpath_out = str(
myjckt.InputandDriverpath) + os.sep + str(Base_name) + ".SD.out"
myjckt.Readpath_sum = str(
myjckt.InputandDriverpath) + os.sep + str(Base_name) + ".SD.sum"
myjckt.Delete_file = False #Deletes driver, input, and output files. Does not delete Echo file.
#INPUT FILE INPUTS----------------------------------------------------------
#Simulation Control
myjckt.Echo = np.array(
[False, "Echo", "- Echo input data to "
"<rootname>.SD.ech"
" (flag)"])
myjckt.SDdeltaT = np.array([
"DEFAULT", "SDdeltaT", "- Local Integration Step. If "
"default"
", the glue-code integration step will be used."
])
myjckt.IntMethod = np.array(
[4, "IntMethod", "- Integration Method [1/2/3/4 = RK4/AB4/ABM4/AM2]."])
myjckt.SttcSolve = np.array([
False, "SttcSolve", "- Solve dynamics about static equilibrium point"
])
#FEA and CRAIG-BAMPTON PARAMETERS
myjckt.FEMmod = np.array([
3,
"- FEM switch: element model in the FEM. [1= Euler-Bernoulli(E-B); 2=Tapered E-B (unavailable); 3= 2-node Timoshenko; 4= 2-node tapered Timoshenko (unavailable)]"
])
myjckt.NDiv = np.array(
[1, "NDiv", "- Number of sub-elements per member"]
) #CJB "HARDWIRED" INTO PYSUBDYN AS 1 TO ALLOW JACKETSE'S NODES TO BE USED AS SUBDYN'S JOINTS
myjckt.CBMod = np.array([
False,
"- [T/F] If True perform C-B reduction, else full FEM dofs will be retained. If True, select Nmodes to retain in C-B reduced system."
])
myjckt.Nmodes = np.array([
75,
"- Number of internal modes to retain (ignored if CBMod=False). If Nmodes=0 --> Guyan Reduction."
])
myjckt.JDampings = np.array([
2, "JDampings",
"- Damping Ratios for each retained mode (% of critical) If Nmodes>0, list Nmodes structural damping ratios for each retained mode (% of critical), or a single damping ratio to be applied to all retained modes. (last entered value will be used for all remaining modes)."
])
#Structure Joints
myjckt.SDjointsHeader = np.array([[
'JointID', 'JointXss', 'JointYss', 'JointZss',
'[Coordinates of Member joints in SS-Coordinate System]'
], ['(-)', '(m)', '(m)', '(m)']])
#Base Reaction Joints
myjckt.BaseRxnJointsHeader = np.array([[
'RJointID', 'RctTDXss', 'RctTDYss', 'RctTDZss', 'RctRDXss', 'RctRDYss',
'RctRDZss', '[Global Coordinate System]'
], ['(-)', ('flag'), ('flag'), ('flag'), ('flag'), ('flag'), ('flag')]])
#Interface Joints
myjckt.InterfaceRxnJointsHeader = np.array([[
'IJointID', 'ItfTDXss', 'ItfTDYss', 'ItfTDZss', 'ItfRDXss', 'ItfRDYss',
'ItfRDZss', '[Global Coordinate System]'
], ['(-)', ('flag'), ('flag'), ('flag'), ('flag'), ('flag'), ('flag')]])
#Members
myjckt.MembersHeader = np.array([[
'MemberID', 'MJointID1', 'MJointID2', 'MPropSetID1', 'MPropSetID2',
'COSMID'
], ['(-)', '(-)', '(-)', '(-)', '(-)', '(-)']])
#MEMBER X-SECTION PROPERTY data 1/2
myjckt.NPropSets = np.array([
6, 'NPropSets',
'- # of structurally unique x-sections (i.e. # of X-sectional props utilized throughout all of the members)'
])
myjckt.PropSet1Header = np.array(
[['PropSetID', 'YoungE', 'ShearG', 'MatDens', 'XsecD', 'XsecT'],
['(-)', '(N/m2)', '(N/m2)', '(kg/m3)', '(m)', '(m)']])
#MEMBER X-SECTION PROPERTY data 2/2
myjckt.PropSet2 = np.array([])
myjckt.PropSet2Header = np.array([[
"PropSetID", "YoungE", "ShearG", "MatDens", "XsecA", "XsecAsx",
"XsecAsy", "XsecJxx", "XsecJyy", "XsecJ0"
],
[
"(-)", "(N/m2)", "(N/m2)", "(kg/m3)",
"(m2)", "(m2)", "(m2)", "(m4)",
"(m4)", "(m4)"
]])
#MEMBER COSINE MATRICES COSM(i,j)
myjckt.COSMHeader = np.array([[
"COSMID", "COSM11", "COSMID12", "COSMID13", "COSMID21", "COSMID22",
"COSMID23", "COSMID31", "COSMID32", "COSMID33"
], ["(-)", "(-)", "(-)", "(-)", "(-)", "(-)", "(-)", "(-)", "(-)", "(-)"]])
myjckt.COSMs = np.array([])
#JOINT ADDITIONAL CONCENTRATED MASSES
myjckt.CmassHeader = np.array(
[["CMJointID", "JMass", "JMXX", "JMYY", "JMZZ"],
["(-)", "(kg)", "(kg*m^2)", "(kg*m^2)", "(kg*m^2)"]])
myjckt.Cmass = np.array([])
#OUTPUT: SUMMARY & OUTFILE
myjckt.SSSum = np.array([
True, "SSSum",
"- Output a Summary File (flag).It contains: matrices K,M and C-B reduced M_BB, M-BM, K_BB, K_MM(OMG^2), PHI_R, PHI_L. It can also contain COSMs if requested."
])
myjckt.OutCOSM = np.array([
True, "OutCOSM",
"- Output cosine matrices with the selected output member forces (flag)"
])
myjckt.OutAll = np.array(
[True, "OutAll", "- [T/F] Output all members' end forces "])
myjckt.OutSwtch = np.array([
1, "OutSwtch",
"- [1/2/3] Output requested channels to: 1=<rootname>.SD.out; 2=<rootname>.out (generated by FAST); 3=both files."
])
myjckt.TabDelim = np.array([
True, "TabDelim",
"- Generate a tab-delimited output in the <rootname>.SD.out file"
])
myjckt.OutDec = np.array(
[1, "OutDec", "- Decimation of output in the <rootname>.SD.out file"])
myjckt.OutFmt = np.array([
"Es11.4e2", "OutFmt",
"- Output format for numerical results in the <rootname>.SD.out file"
])
myjckt.OutSFmt = np.array([
"A11", "OutFmt",
"- Output format for header strings in the <rootname>.SD.out file"
])
#MEMBER OUTPUT LIST
myjckt.MemOutListHeader=np.array([['MemberID','NoutCnt','NodeCnt','[NOutCnt=how many nodes to get output for [< 10]; NodeCnt are local ordinal numbers from the start of the member, and must be >=1 and <= NDiv+1] If NMOutputs=0 leave blank as well.]'],\
['(-)','(-)','(-)']])
#SSOutline
myjckt.SSOutlist=np.array([["ReactFXss, ReactFYss, ReactFZss, ReactMXss, ReactMYss, ReactMZss",'-Base reactions (forces onto SS structure)'],\
["IntfFXss, IntfFYss, IntfFZss, IntfMXss, IntfMYss, IntfMZss",'-Interface reactions (forces from SS structure)'],\
["IntfTDXss, IntfTDYss, IntfTDZss, IntfRDXss, IntfRDYss, IntfRDZss",'-Interface deflections '],\
["IntfTAXss, IntfTAYss, IntfTAZss, IntfRAXss, IntfRAYss, IntfRAZss",'Interface accelerations']])
myjckt.InterfaceJointsFlags = np.array([[5, 1, 1, 1, 1, 1, 1]])
myjckt.MemOutList = np.array([[1, 2, 1, 2]])
#DRIVER INPUTS--------------------------------------------------------------
myjckt.EchoD = np.array(
[True, "Echo", "- Echo the input file data (flag)"])
#Environmental Conditions
myjckt.Gravity = np.array([9.81, "Gravity", "- Gravity (m/s^2)"])
myjckt.WtrDpth = np.array(
[43.127, "WtrDpth", "- Water Depth (m) positive value"])
#SubDyn
myjckt.SDInputFile = np.array([myjckt.InputFile_path, "SDInputFile"])
myjckt.OutRootName = np.array([
str(myjckt.InputandDriverpath) + os.sep + str(Base_name), "OutRootName"
])
myjckt.NSteps = np.array(
[600, "NSteps", "- Number of time steps in the simulations (-)"])
myjckt.TimeInterval = np.array(
[0.005, "TimeInterval", "- TimeInterval for the simulation (sec)"])
myjckt.TP_RefPoint = np.array([
0.0, 0.0, 18.15, "TP_RefPoint",
"- Location of the TP reference point in global coordinates (m)"
])
myjckt.SubRotateZ = np.array([
0.0, "SubRotateZ",
"- Rotation angle of the structure geometry in degrees about the global Z axis."
])
#INPUTS
myjckt.InputsMod = np.array([
1, "InputsMod",
"- Inputs model {0: all inputs are zero for every timestep, 1: steadystate inputs, 2: read inputs from a file (InputsFile)} (switch)"
])
myjckt.InputsFile = np.array(
['""', "InputsFile", "- Name of the inputs file if InputsMod = 2"])
#STEADY INPUTS
myjckt.uTPInSteady = np.array([
0.1, 0.0, 0.0, 0.0, 0.0, 0.0, "uTPInSteady",
"- input displacements and rotations ( m, rads )"
])
myjckt.uDotTPInSteady = np.array([
0.0, 0.0, 0.0, 0.0, 0.0, 0.0, "uDotTPInSteady",
"- input translational and rotational velocities ( m/s, rads/s)"
])
myjckt.uDotDotTPInSteady = np.array([
0.0, 0.0, 0.0, 0.0, 0.0, 0.0, "uDotDotTPInSteady",
"- input translational and rotational accelerations ( m/s^2, rads/s^2)"
])
#myjckt.SDpySubDynA.run()
myjckt.JcktGeoIn = Jcktins
myjckt.Soilinputs = Soilinputs
myjckt.Waterinputs = Waterinputs
myjckt.Windinputs = Windinputs
myjckt.Pileinputs = Pileinputs
myjckt.leginputs = leginputs
myjckt.legbot_stmphin = legbot_stmphin #Distance from bottom of leg to second joint along z; must be>0
myjckt.Xbrcinputs = Xbrcinputs
myjckt.Mbrcinputs = Mbrcinputs
myjckt.Hbrcinputs = Hbrcinputs
myjckt.TPlumpinputs = TPlumpinputs
myjckt.TPinputs = TPinputs
myjckt.Twrinputs = Twrinputs
myjckt.TwrRigidTop = TwrRigidTop #Account for RNA via math rather than a physical rigidmember
myjckt.RNAinputs = RNAins
myjckt.RNA_F = RNA_F
myjckt.FrameAuxIns = FrameAuxIns
return myjckt, f0, f0epsilon, jcktDTRmin, mxftprint, guesses, bounds.T
def main(): #\
"""Function to Instantiate a JacketSE Assembly: \n
INPUTS \n
All hardwired, so edit the quantities below all the way to the line "#________________ DO NOT MODIFY THE FOLLOWING ________________#" \n
-See JacketOpt_PyOPT for more information. \n
OUTPUTS \n
myjckt -jacket assembly instance \n\n
Optimization parameters: \n\n
f0 -float, target frequency [Hz]
f0epsilon -float, f0*(1+f0epsilon) will not be exceeded \n
jcktDTRmin -Float, minimum jacket member DTR allowed, mostly for 60+waterdepths. \n
mxftprint -Float, max allowed foot print [m]
guesses -Float(n), guesses for all design variables check out DesVar class. \n
bounds -Float(n,2), bounds for all design variables check out DesVar class. \n\n
SAMPLE CALLS: \n
1.OPTIMIZATION: python JacketOpt_ExtCobyla.py C:\RRD\PYTHON\WISDEM\JacketSE\src\jacketse\MyJacketInputs.py \n
2.OPTIMIZATION: python JacketOpt_PyOPT.py C:\RRD\PYTHON\WISDEM\JacketSE\src\jacketse\MyJacketInputs.py True \n
3.BUILD JACKET: python >>> myjacket=C:\RRD\PYTHON\WISDEM\JacketSE\src\jacketse\MyJacketInputs.py \n
"""
#Set inputs ###----ALL USER INPUT----###
Jcktins=JcktGeoInputs()
Jcktins.nlegs =4
Jcktins.nbays =4 #CJB To change this you must change tleg, below
Jcktins.batter=30.5495 #=(-43.127+24.614)/(5.939-5.333)
#Jcktins.dck_botz =15.651
Jcktins.dck_botz =16.51 #CJBe
Jcktins.dck_width= 8.+1.2
Jcktins.weld2D = 0.
Jcktins.VPFlag = True #vertical pile T/F; to enable piles in frame3DD set pileinputs.ndiv>0
Jcktins.clamped= True #whether or not the bottom of the structure is rigidly connected. Use False when equivalent spring constants are being used.
Jcktins.AFflag = False #whether or not to use apparent fixity piles
Jcktins.PreBuildTPLvl = 0 #if >0, the TP is prebuilt according to rules per PreBuildTP
#______________________________________________#
#Soil inputs
Soilinputs=SoilGeoInputs()
Soilinputs.zbots =-np.array([3.,5.,7.,15.,30.,50.])
Soilinputs.gammas =np.array([10000.,10000.,10000.,10000.,10000.,10000.])
Soilinputs.cus =np.array([60000.,60000.,60000.,60000.,60000.,60000.])
Soilinputs.phis =np.array([26.,26.,26.,26.,26.,26])#np.array([36.,33.,26.,37.,35.,37.5])#np.array([36.,33.,26.,37.,35.,37.5])
Soilinputs.delta =25.
Soilinputs.sndflg =True
Soilinputs.PenderSwtch =False #True
Soilinputs.SoilSF =1.
#______________________________________________#
#Water and wind inputs
#Water and wind inputs
Waterinputs=WaterInputs() #CJBtest Max thrust case
Waterinputs.wdepth =50. #CJBtest Max thrust case
Waterinputs.wlevel =50. #CJBtest Max thrust case #Distance from bottom of structure to surface THIS, I believe is no longer needed as piles may be negative in z, to check and remove in case
Waterinputs.T=12. #CJBtest Max thrust case #Wave Period
Waterinputs.HW=10 #CJBtest Max thrust case #Wave Height
Waterinputs.Cd=3. #CJBtest Max thrust case #Drag Coefficient, enhanced to account for marine growth and other members not calculated
Waterinputs.Cm=8.#2. #CJBtest Max thrust case #Added mass Coefficient
#WaterInputs.Uc=0.0 #CJBtest Max thrust case test
Windinputs=WindInputs() #CJBtest Max thrust case
Windinputs.HH=87.6+.51+Jcktins.dck_botz+4 #CJBtest Max thrust case (4 comes from the height of the TP) #CHECK HOW THIS COMPLIES....
Windinputs.Cdj=4. #CJBtest Max thrust case #Drag Coefficient for jacket members, enhanced to account for TP drag not calculated otherwise
Windinputs.Cdt=2 #CJBtest Max thrust case #Drag Coefficient for tower, enhanced to account for TP drag not calculated otherwise
Windinputs.al_shear=.2 #CJBtest Max thrust case test
Windinputs.U50HH=20 #CJBtest Max thrust case test #assumed gust speed
#Windinputs.U50HH=70. #CJBtest Max wind speed case test #assumed gust speed
#______________________________________________#
#Pile data
Pilematin=MatInputs()
Pilematin.matname=np.array(['steel']) #CJB Changed this from RC into steel
Pilematin.E=np.array([ 2.1e11])
Pilematin.G=np.array([8.07690e+10])
Pilematin.rho=np.array([3339.12]) *34274.82/36876. #From Test04.txt in SD, to check with official FAST certtest
Pileinputs=PileGeoInputs()
Pileinputs.Pilematins=Pilematin
Pileinputs.ndiv=0 #CJB Change this from 1 to 0 #3 ###----USER INPUT----###
Pileinputs.Dpile=2.082
Pileinputs.tpile=0.491
Pileinputs.Lp=0. #[m] Embedment length
#______________________________________________#
#Legs data
legmatin=MatInputs()
legmatin.matname=(['steel'])
legmatin.rho=np.array([7850.])
Dleg=np.asarray([1.2]).repeat(Jcktins.nbays+1) #e.g., np.array([2.0,1.8,1.6,1.6,1.6])
tleg=np.asarray([0.05,0.05,0.035,0.035,0.035]) #CJB Length must be 1 more than (nbays)
leginputs=LegGeoInputs()
leginputs.legZbot = 4.5 ###----USER INPUT----###
leginputs.ndiv=1 ###----USER INPUT----###
leginputs.legmatins=legmatin
leginputs.Dleg=Dleg
leginputs.tleg=tleg
#The following is a passthrough variables
legbot_stmphin =(45.5-43.127) #=2.373 Distance from bottom of leg to second joint along z; must be>0
#______________________________________________#
#Xbrc data
Xbrcmatin=MatInputs()
Xbrcmatin.matname=np.array(['steel']).repeat(Jcktins.nbays)
Xbrcmatin.rho=np.array([7850.])
Dbrc=np.asarray([0.8]).repeat(Jcktins.nbays)
tbrc=np.asarray([0.02]).repeat(Jcktins.nbays)
Xbrcinputs=XBrcGeoInputs()
Xbrcinputs.Dbrc=Dbrc
Xbrcinputs.tbrc=tbrc
Xbrcinputs.ndiv=1 ###----USER INPUT----###
Xbrcinputs.Xbrcmatins=Xbrcmatin
Xbrcinputs.precalc=False #This can be set to true if we want Xbraces to be precalculated in D and t, in which case the above set Dbrc and tbrc would be overwritten
#______________________________________________#
#Mbrc data
Mbrcmatin=MatInputs()
Mbrcmatin.matname=np.array(['steel'])
Mbrcmatin.rho=np.array([7850.])
Mbrcinputs=MudBrcGeoInputs()
Mbrcinputs.Dbrc_mud=0.8 ###----USER INPUT----###
Mbrcinputs.tbrc_mud=0.02
Mbrcinputs.ndiv=2 ###----USER INPUT----###
Mbrcinputs.Mbrcmatins=Mbrcmatin
Mbrcinputs.precalc=False #This can be set to true if we want Mudbrace to be precalculated in D and t, in which case the above set Dbrc_mud and tbrc_mud would be overwritten
#______________________________________________#
#Hbrc data
Hbrcmatin=MatInputs()
Hbrcmatin.matname=np.array(['steel'])
Hbrcmatin.rho=np.array([7850.])
Dbrc_hbrc=1.1 ###----USER INPUT----###
Hbrcinputs=HBrcGeoInputs()
Hbrcinputs.Dbrch=Dbrc_hbrc ###----USER INPUT----###
Hbrcinputs.ndiv=0
Hbrcinputs.Hbrcmatins=Hbrcmatin
Hbrcinputs.precalc=True #This can be set to true if we want Hbrace to be set=Xbrace top D and t, in which case the above set Dbrch and tbrch would be overwritten
#______________________________________________#
#TP data
#Note PrebuildTPLvl is set in JacketIns ###----USER INPUT----###
#TP lumped mass data
TPlumpinputs=TPlumpMass() ###----ALL USER INPUT----###
TPlumpinputs.mass = 666.e3#-98385.33+( 7850.*4*np.pi/4.*(1.2**2-(1.2-2.*0.04)**2)*4) #[kg] TO MODIFY AFTER WE ASSESS OVERALL TP MASS, to be reduced for the steel weight
TPlumpinputs.CMoff= np.array([0.,0.,2.]) #CG of concrete block is 2 m above intersection of diagonal braces
TPlumpinputs.I = 1./12*TPlumpinputs.mass*np.array([8.**2+4.**2,8.**2+4.**2,8.**2+8.**2,0.,0.,0.])
TPstrtmatin=MatInputs()
TPstmpsmatin=MatInputs()
TPgirdmatin=MatInputs()
TPbrcmatin=MatInputs()
TPstemmatin=MatInputs()
TPstmpsmatin.matname=np.array(['steel'])
TPstmpsmatin.rho=np.array([7850.])
TPstrtmatin.matname=np.array(['steel'])
TPstrtmatin.rho=np.array([1350.])
TPbrcmatin.matname=np.array(['steel'])
TPbrcmatin.rho=np.array([1350.])#np.array([7850.]) tpstrucmass=np.pi/4*(1.2**2-(1.2-2*0.04)**2)*7850*4*4 7850.*tpstrucmass/myjckt.TP.TPouts.mass=1462.185
TPgirdmatin.matname=np.array(['steel'])
TPgirdmatin.rho=np.array([1350.])
TPstemmatin.matname=np.array(['steel']).repeat(2) ###----ALL USER INPUT----###
TPstemmatin.rho=np.array([1350.])
TPinputs=TPGeoInputs()
TPinputs.TPstrtmatins=TPstrtmatin
TPinputs.TPbrcmatins=TPbrcmatin
TPinputs.TPstemmatins=TPstemmatin
TPinputs.TPstmpmatins=TPstmpsmatin
TPinputs.TPgirdmatins=TPgirdmatin
#Set TP dimensions as leg and brace dimensions
TPinputs.Dstrut=1.2 ###----ALL USER INPUT----###
TPinputs.tstrut=0.04
TPinputs.Dgir=TPinputs.Dstrut
TPinputs.tgir=TPinputs.tstrut
TPinputs.Dbrc=TPinputs.Dstrut
TPinputs.tbrc=TPinputs.tstrut
###----ALL USER INPUT----###
TPinputs.hstump=0.499#(16.15-15.651)
TPinputs.Dstump=1.2
TPinputs.tstump=0.04
TPinputs.stumpndiv=1
TPinputs.brcndiv=1
TPinputs.girndiv=1
TPinputs.strutndiv=1
TPinputs.stemndiv=1
TPinputs.nstems=3
TPinputs.Dstem=np.array([5.6]).repeat(TPinputs.nstems)
TPinputs.tstem=np.array([0.032,0.032,0.032])
TPinputs.hstem=np.array([(4.)/TPinputs.nstems]).repeat(TPinputs.nstems)
#______________________________________________#
#Tower data
Twrmatin=MatInputs()
Twrmatin.matname=np.array(['heavysteel']) #CJBtest
Twrmatin.rho=np.array([8500.]) #CJBtest
#Twrmatin.matname=np.array(['steel'])
#Twrmatin.rho=np.array([7850.])
Twrinputs=TwrGeoInputs()
Twrinputs.Twrmatins=Twrmatin
#Twrinputs.Htwr=88.15 #Trumped by HH
Twrinputs.Htwr2frac=1./87.6 #CJBtest #fraction of tower height with constant x-section
Twrinputs.ndiv=np.array([1,1]) #ndiv for uniform and tapered section ###----USER INPUT----###
Twrinputs.DeltaZmax= 5. #[m], maximum FE element length allowed in the tower members (i.e. the uniform and the tapered members)
Twrinputs.Db=6. #CJBtest
Twrinputs.DTRb=Twrinputs.Db/(1.3*.027) #CJBtest
Twrinputs.Dt=3.87 #CJBtest
Twrinputs.DTRt=Twrinputs.Dt/(1.3*.019) #CJBtest
#Set whether or not DTRb and DTRt for the tower are the same. Note if next set to False it will trump DTRt setting above
Twrinputs.DTRsdiff=True ##SET THIS TO TRUE IF YOU WANT DTRs to be different between base and top
#If you use the following 12 lines, The geometry defined above is ignored
#CJBtest Don't use stations
#ztwr=np.array([20.15,21.15,32.15,42.15,54.15,64.15,74.15,83.15,88.15]) -20.15
#Dtwr=np.array([5.6,5.577,5.318,5.082,4.8,4.565,4.329,4.118,4])
#ttwr=np.array([0.032,0.032,0.03,0.028,0.024,0.022,0.02,0.03,0.03])
#pmtwr=np.array([ np.array([20.15,54.15,88.15])-20.15,[1.9e3,1.4e3,1.0e3]]).T #(3,2) first col z's, second weights
#Interpolate data to refine tower discretization
#dz=1. #[m] maximum deltaz allowed in discretization
#ztwr2=np.linspace(ztwr[0],ztwr[-1],round((ztwr[-1]-ztwr[0])/dz)) #New discretization
#Dtwr_interp=interp1d(ztwr,Dtwr)
#ttwr_interp=interp1d(ztwr,ttwr)
#Twrinputs.ztwr=ztwr2
#Twrinputs.Dtwr=Dtwr_interp(ztwr2)
#Twrinputs.ttwr=ttwr_interp(ztwr2)
#Twrinputs.TwrlumpedMass=np.zeros([pmtwr.shape[0],11])
#Twrinputs.TwrlumpedMass[:,0:2]=pmtwr
TwrRigidTop=False #False=Account for RNA via math rather than a physical rigidmember
#______________________________________________#
#RNA data
RNAins=RNAprops()
RNAins.mass=350.e3 #CJBtest #[kg]
RNAins.I[0]=114930678 #CJBtest #[kg m2]
RNAins.I[1]=22035403 #CJBtest #[kg m2]
RNAins.I[2]=18759742.50 #CJBtest #[kg m2]
RNAins.I[4]=503710.47 #CJBtest #[kg m2]
RNAins.CMoff[0]=-1.13 #CJBtest #[m]
RNAins.CMoff[2]=.51 #CJBtest #[m]
#RNAins.Thoff[2]=2.4 #CJBtest #[m]
RNAins.yawangle=0. #CJBtest #angle with respect to global X, CCW looking from above, wind from left
RNAins.rna_weightM=True
UtilAssembly.tilt=5.0 #CJBtest test
#______________________________________________#
#RNA loads Fx-z, Mxx-zz
RNA_F=np.array([1284744.196,0.,-112400.5527,3963732.762,896380.8464,-346781.6819]) #CJBtest Max thrust case #unfactored thrust, though accounting for gust and dynamic effects (no IEC PSF though)
#RNA_F=np.array([188038.8045,0.,-16451.2637,0.0,131196.8431,0.0]) #CJBtest Max wind speed case #unfactored thrust, though accounting for gust and dynamic effects (no IEC PSF though)
#RNA_F=np.array([1000.e3,0.,0.,0.,0.,0.])
#______________________________________________#
# Frame3DD parameters ###----ALL USER INPUT----###
FrameAuxIns=Frame3DDaux()
FrameAuxIns.sh_fg=1 #shear flag-->Timoshenko
FrameAuxIns.deltaz=5.
FrameAuxIns.geo_fg=0
FrameAuxIns.nModes = 6 # number of desired dynamic modes of vibration
FrameAuxIns.Mmethod = 1 # 1: subspace Jacobi 2: Stodola
FrameAuxIns.lump = 0 # 0: consistent mass ... 1: lumped mass matrix
FrameAuxIns.tol = 1e-9 # mode shape tolerance
FrameAuxIns.shift = 0.0 # shift value ... for unrestrained structures
FrameAuxIns.gvector=np.array([0.,0.,-9.8065]) #GRAVITY
#Decide whether or not to consider DLC 6.1 as well
twodlcs=False
#______________________________________________#
#______________________________________________#
# OTHER AUXILIARY CONSTRAINTS AND TARGETS FOR OPTIMIZATION #
#______________________________________________#
#______________________________________________#
#Set Optimization Bounds and guesses for the various variables:
# x= [ batter, Dpile, tpile, Lp, Dleg, tleg, Dbrc, tbrc, Dbrc_mud, tbrc_mud, Dgit, tgir, Db, DTRb Dt, DTRt Htwr2fac dck_widthfact]
MnCnst = np.array([ 8., 1., 1.*0.0254, 20., 1., 1.*0.0254, 1., 1.*0.0254, 1., 1.*0.0254, 1., 1.*0.0254, 5., 120., 3., 120., 0.05, 2.])
MxCnst = np.array([ 15., 2.5, 5.*0.0254, 50., 2.5, 5.*0.0254, 2., 5.*0.0254, 2., 5.*0.0254, 2., 5.*0.0254, 7., 200., 4., 200., 0.25, 3.])
guesses= np.array([ 10., 1.5, 1.5*0.0254, 26., 1.8, 1.5*0.0254, 1.2, 1.5*0.0254, 1.2, 1.5*0.0254, 1.2, 1.5*0.0254, 6., 140., 3.5, 150., 0.2, 2.])
#SET Maximum Footprint [m]
mxftprint =30.
#Set target frequency [Hz] and f0epsilon, i.e. fmax=(1+f0eps)*f0
f0=0.22
f0epsilon=0.1
#Set the minminimum DTR allowed for jacket members; mostly for 60+waterdepths
jcktDTRmin=22.
#_____________________________________________________________#
#________________ DO NOT MODIFY THE FOLLOWING ________________#
#_____________________________________________________________#
bounds=np.vstack((MnCnst,MxCnst))
desvarmeans=np.mean(bounds,1)
# Now Launch the assembly and pass all of the inputs
#myjckt=set_as_top(JacketSE(Jcktins.clamped,Jcktins.AFflag,twodlcs=twodlcs, wlevel_Ulist=29))#CJB and JQ
myjckt=set_as_top(JacketSE(Jcktins.clamped,Jcktins.AFflag,twodlcs=twodlcs))
#pySubDyn Parameters CJB+
#SDpySubDynA = pySubDynA()
#INPUTS TO RUN SUBDYN-------------------------------------------------------
#(PATH INFORMATION FOR INPUT FILE AND DRIVER)
Base_name="5MW_Tower_JEnv_pySubDyn" #Input name here
#INPUT FILE PATH
myjckt.InputFile_name=str(Base_name)+".txt"
#myjckt.SDpySubDynA.InputFile_name=str(Base_name)+".txt"
myjckt.InputandDriverpath="C:\wisdem\plugins\JacketSE\src\jacketse\SubDyn\CertTest"
myjckt.InputFile_path=myjckt.InputandDriverpath+os.sep+str(myjckt.InputFile_name)
#DRIVER PATH
myjckt.Driver_name=str(Base_name)+"D"+".txt"
myjckt.Driver_path=myjckt.InputandDriverpath+os.sep+str(myjckt.Driver_name)
myjckt.Driver_path=myjckt.InputandDriverpath+os.sep+str(myjckt.Driver_name)
#PATH TO RUN SUBDYN
SDEXEpath="C:\wisdem\plugins\JacketSE\src\jacketse\SubDyn"+os.sep+"bin\SubDyn_Win32.exe"
myjckt.SDpath=str(SDEXEpath)+' '+str(myjckt.Driver_path)
#test.SDpath='r'+"'''"+test.SDEXEpath+' '+test.SDDriverpath+"'''"
#PATH TO READ OUTPUT (INPUTS TO READ OUTPUT)
myjckt.Readpath_out=str(myjckt.InputandDriverpath)+os.sep+str(Base_name)+".SD.out"
myjckt.Readpath_sum=str(myjckt.InputandDriverpath)+os.sep+str(Base_name)+".SD.sum"
myjckt.Delete_file=False #Deletes driver, input, and output files. Does not delete Echo file.
#INPUT FILE INPUTS----------------------------------------------------------
#Simulation Control
myjckt.Echo=np.array([False, "Echo", "- Echo input data to ""<rootname>.SD.ech"" (flag)"])
myjckt.SDdeltaT=np.array(["DEFAULT", "SDdeltaT", "- Local Integration Step. If ""default"", the glue-code integration step will be used."])
myjckt.IntMethod=np.array([4, "IntMethod", "- Integration Method [1/2/3/4 = RK4/AB4/ABM4/AM2]."])
myjckt.SttcSolve=np.array([False, "SttcSolve", "- Solve dynamics about static equilibrium point"])
#FEA and CRAIG-BAMPTON PARAMETERS
myjckt.FEMmod=np.array([3, "- FEM switch: element model in the FEM. [1= Euler-Bernoulli(E-B); 2=Tapered E-B (unavailable); 3= 2-node Timoshenko; 4= 2-node tapered Timoshenko (unavailable)]"])
myjckt.NDiv=np.array([1, "NDiv", "- Number of sub-elements per member"])#CJB "HARDWIRED" INTO PYSUBDYN AS 1 TO ALLOW JACKETSE'S NODES TO BE USED AS SUBDYN'S JOINTS
myjckt.CBMod=np.array([False, "- [T/F] If True perform C-B reduction, else full FEM dofs will be retained. If True, select Nmodes to retain in C-B reduced system."])
myjckt.Nmodes=np.array([75, "- Number of internal modes to retain (ignored if CBMod=False). If Nmodes=0 --> Guyan Reduction."])
myjckt.JDampings=np.array([2, "JDampings", "- Damping Ratios for each retained mode (% of critical) If Nmodes>0, list Nmodes structural damping ratios for each retained mode (% of critical), or a single damping ratio to be applied to all retained modes. (last entered value will be used for all remaining modes)."])
#Structure Joints
myjckt.SDjointsHeader=np.array([['JointID','JointXss','JointYss','JointZss','[Coordinates of Member joints in SS-Coordinate System]'], ['(-)','(m)','(m)','(m)']])
#Base Reaction Joints
myjckt.BaseRxnJointsHeader=np.array([['RJointID','RctTDXss','RctTDYss','RctTDZss','RctRDXss','RctRDYss','RctRDZss','[Global Coordinate System]'], ['(-)',('flag'),('flag'),('flag'),('flag'),('flag'),('flag')]])
#Interface Joints
myjckt.InterfaceRxnJointsHeader=np.array([['IJointID','ItfTDXss','ItfTDYss','ItfTDZss','ItfRDXss','ItfRDYss','ItfRDZss','[Global Coordinate System]'], ['(-)',('flag'),('flag'),('flag'),('flag'),('flag'),('flag')]])
#Members
myjckt.MembersHeader=np.array([['MemberID','MJointID1','MJointID2','MPropSetID1','MPropSetID2','COSMID'], ['(-)','(-)','(-)','(-)','(-)','(-)']])
#MEMBER X-SECTION PROPERTY data 1/2
myjckt.NPropSets=np.array([6, 'NPropSets', '- # of structurally unique x-sections (i.e. # of X-sectional props utilized throughout all of the members)'])
myjckt.PropSet1Header=np.array([['PropSetID', 'YoungE', 'ShearG', 'MatDens', 'XsecD', 'XsecT'],['(-)', '(N/m2)', '(N/m2)', '(kg/m3)', '(m)', '(m)']])
#MEMBER X-SECTION PROPERTY data 2/2
myjckt.PropSet2=np.array([])
myjckt.PropSet2Header=np.array([["PropSetID","YoungE","ShearG","MatDens","XsecA","XsecAsx","XsecAsy","XsecJxx","XsecJyy","XsecJ0"],["(-)","(N/m2)","(N/m2)","(kg/m3)","(m2)","(m2)","(m2)","(m4)","(m4)","(m4)"]])
#MEMBER COSINE MATRICES COSM(i,j)
myjckt.COSMHeader=np.array([["COSMID","COSM11","COSMID12","COSMID13","COSMID21","COSMID22","COSMID23","COSMID31","COSMID32","COSMID33"],["(-)","(-)","(-)","(-)","(-)","(-)","(-)","(-)","(-)","(-)"]])
myjckt.COSMs=np.array([])
#JOINT ADDITIONAL CONCENTRATED MASSES
myjckt.CmassHeader=np.array([["CMJointID","JMass","JMXX","JMYY","JMZZ"],["(-)","(kg)" ,"(kg*m^2)","(kg*m^2)","(kg*m^2)"]])
myjckt.Cmass=np.array([])
#OUTPUT: SUMMARY & OUTFILE
myjckt.SSSum=np.array([True, "SSSum", "- Output a Summary File (flag).It contains: matrices K,M and C-B reduced M_BB, M-BM, K_BB, K_MM(OMG^2), PHI_R, PHI_L. It can also contain COSMs if requested."])
myjckt.OutCOSM=np.array([True, "OutCOSM", "- Output cosine matrices with the selected output member forces (flag)"])
myjckt.OutAll=np.array([True, "OutAll", "- [T/F] Output all members' end forces "])
myjckt.OutSwtch=np.array([1, "OutSwtch", "- [1/2/3] Output requested channels to: 1=<rootname>.SD.out; 2=<rootname>.out (generated by FAST); 3=both files."])
myjckt.TabDelim=np.array([True, "TabDelim", "- Generate a tab-delimited output in the <rootname>.SD.out file"])
myjckt.OutDec=np.array([1, "OutDec", "- Decimation of output in the <rootname>.SD.out file"])
myjckt.OutFmt=np.array(["Es11.4e2", "OutFmt", "- Output format for numerical results in the <rootname>.SD.out file"])
myjckt.OutSFmt=np.array(["A11", "OutFmt", "- Output format for header strings in the <rootname>.SD.out file"])
#MEMBER OUTPUT LIST
myjckt.MemOutListHeader=np.array([['MemberID','NoutCnt','NodeCnt','[NOutCnt=how many nodes to get output for [< 10]; NodeCnt are local ordinal numbers from the start of the member, and must be >=1 and <= NDiv+1] If NMOutputs=0 leave blank as well.]'],\
['(-)','(-)','(-)']])
#SSOutline
myjckt.SSOutlist=np.array([["ReactFXss, ReactFYss, ReactFZss, ReactMXss, ReactMYss, ReactMZss",'-Base reactions (forces onto SS structure)'],\
["IntfFXss, IntfFYss, IntfFZss, IntfMXss, IntfMYss, IntfMZss",'-Interface reactions (forces from SS structure)'],\
["IntfTDXss, IntfTDYss, IntfTDZss, IntfRDXss, IntfRDYss, IntfRDZss",'-Interface deflections '],\
["IntfTAXss, IntfTAYss, IntfTAZss, IntfRAXss, IntfRAYss, IntfRAZss",'Interface accelerations']])
myjckt.InterfaceJointsFlags=np.array([[5,1,1,1,1,1,1]])
myjckt.MemOutList=np.array([[1,2,1,2]])
#DRIVER INPUTS--------------------------------------------------------------
myjckt.EchoD=np.array([True, "Echo", "- Echo the input file data (flag)"])
#Environmental Conditions
myjckt.Gravity=np.array([9.81, "Gravity", "- Gravity (m/s^2)"])
myjckt.WtrDpth=np.array([43.127, "WtrDpth", "- Water Depth (m) positive value"])
#SubDyn
myjckt.SDInputFile=np.array([myjckt.InputFile_path, "SDInputFile"])
myjckt.OutRootName=np.array([str(myjckt.InputandDriverpath)+os.sep+str(Base_name), "OutRootName"])
myjckt.NSteps=np.array([600, "NSteps", "- Number of time steps in the simulations (-)"])
myjckt.TimeInterval=np.array([0.005, "TimeInterval", "- TimeInterval for the simulation (sec)"])
myjckt.TP_RefPoint=np.array([0.0, 0.0, 18.15, "TP_RefPoint", "- Location of the TP reference point in global coordinates (m)"])
myjckt.SubRotateZ=np.array([0.0, "SubRotateZ", "- Rotation angle of the structure geometry in degrees about the global Z axis."])
#INPUTS
myjckt.InputsMod=np.array([1, "InputsMod", "- Inputs model {0: all inputs are zero for every timestep, 1: steadystate inputs, 2: read inputs from a file (InputsFile)} (switch)"])
myjckt.InputsFile=np.array(['""', "InputsFile", "- Name of the inputs file if InputsMod = 2"])
#STEADY INPUTS
myjckt.uTPInSteady=np.array([0.1, 0.0, 0.0, 0.0, 0.0, 0.0, "uTPInSteady", "- input displacements and rotations ( m, rads )"])
myjckt.uDotTPInSteady=np.array([0.0, 0.0, 0.0, 0.0, 0.0, 0.0, "uDotTPInSteady", "- input translational and rotational velocities ( m/s, rads/s)"])
myjckt.uDotDotTPInSteady=np.array([0.0, 0.0, 0.0, 0.0, 0.0, 0.0, "uDotDotTPInSteady", "- input translational and rotational accelerations ( m/s^2, rads/s^2)"])
#myjckt.SDpySubDynA.run()
myjckt.JcktGeoIn=Jcktins
myjckt.Soilinputs=Soilinputs
myjckt.Waterinputs=Waterinputs
myjckt.Windinputs=Windinputs
myjckt.Pileinputs=Pileinputs
myjckt.leginputs=leginputs
myjckt.legbot_stmphin =legbot_stmphin #Distance from bottom of leg to second joint along z; must be>0
myjckt.Xbrcinputs=Xbrcinputs
myjckt.Mbrcinputs=Mbrcinputs
myjckt.Hbrcinputs=Hbrcinputs
myjckt.TPlumpinputs=TPlumpinputs
myjckt.TPinputs=TPinputs
myjckt.Twrinputs=Twrinputs
myjckt.TwrRigidTop=TwrRigidTop #Account for RNA via math rather than a physical rigidmember
myjckt.RNAinputs=RNAins
myjckt.RNA_F=RNA_F
myjckt.FrameAuxIns=FrameAuxIns
return myjckt,f0,f0epsilon,jcktDTRmin,mxftprint,guesses,bounds.T
