Lines Matching refs:GetValue
44 if ((string)inp.GetValue("Employ AMG") == "True" ) { in input_fform()
48 amgvari.irun_amg_prec = inp.GetValue("Run AMG As CG-preconditioner"); in input_fform()
50 amgvarr.strong_eps = inp.GetValue("Strong Criterion Eps"); in input_fform()
52 amgvarr.ramg_eps = inp.GetValue("AMG Convergence Eps"); in input_fform()
54 amgvarr.ramg_relax = inp.GetValue("AMG Relaxation Omega"); in input_fform()
55 amgvarr.ramg_trunc = inp.GetValue("AMG Truncation Set"); in input_fform()
57 amgvari.iamg_verb = inp.GetValue("AMG Verbosity"); in input_fform()
59 amgvari.iamg_neg_sten = inp.GetValue("AMG Neg_Sten"); in input_fform()
61 amgvari.iamg_nlevel = inp.GetValue("AMG Nlevel"); in input_fform()
63 amgvari.iamg_c_solver = inp.GetValue("AMG Coarsest Solver"); in input_fform()
66 amgvari.iamg_setup_frez = inp.GetValue("AMG Freeze Setup"); in input_fform()
67 if ((string)inp.GetValue("AMG Interpolation Type")=="Standard") in input_fform()
71 amgvari.maxnev = inp.GetValue("AMG GGB nev"); in input_fform()
72 amgvari.maxncv = inp.GetValue("AMG GGB ncv"); in input_fform()
74 if ((string)inp.GetValue("AMG Smoother Type")=="Gauss-Seidel") in input_fform()
76 else if ((string)inp.GetValue("AMG Smoother Type")=="ChebyShev") in input_fform()
78 else if ((string)inp.GetValue("AMG Smoother Type")=="MLS") in input_fform()
80 amgvarr.ramg_chebyratio = inp.GetValue("AMG Chebyshev Eigenvalue ratio"); in input_fform()
82 amgvari.mlsdeg = inp.GetValue("AMG MLS Degree"); in input_fform()
83 amgvari.iamg_reduce = inp.GetValue("AMG Run Reduced Serial"); in input_fform()
89 ctrlvari.iI2Binlet = (int)inp.GetValue("Take BC from IC at Inlet"); in input_fform()
92 ctrlvar.inletVelX = inp.GetValue("Inlet Bulk x Velocity"); in input_fform()
98 ductvari.isetOutletID = (int)inp.GetValue("Duct Outlet ID"); in input_fform()
100 ctrlvar.outPres1 = inp.GetValue("Duct Uniform Outlet Pressure"); in input_fform()
103 ductvari.isetEV_IC_BC=(int)inp.GetValue("Override Eddy Viscosity"); in input_fform()
105 ductvar.evis_IC_BC=inp.GetValue("Eddy Viscosity Value for Override"); in input_fform()
108 if(ductvari.isetEVramp = (int)inp.GetValue("Specify Initial Eddy Viscosity Ramp")){ in input_fform()
109 ductvar.EVrampXmin =inp.GetValue("Initial Scalar 1 ramp start"); in input_fform()
110 ductvar.EVrampXmax =inp.GetValue("Initial Scalar 1 ramp end"); in input_fform()
111 ductvar.EVrampMax =inp.GetValue("Initial Scalar 1 high"); in input_fform()
112 ductvar.EVrampMin =inp.GetValue("Initial Scalar 1 low"); in input_fform()
116 ctrlvari.isetInitial=(int)inp.GetValue("Specify Initial Conditions"); in input_fform()
118 ctrlvar.xvel_ini = inp.GetValue("Initial X Velocity"); in input_fform()
119 ctrlvar.yvel_ini = inp.GetValue("Initial Y Velocity"); in input_fform()
120 ctrlvar.zvel_ini = inp.GetValue("Initial Z Velocity"); in input_fform()
121 ctrlvar.temp_ini = inp.GetValue("Initial Temp"); in input_fform()
122 ctrlvar.pres_ini = inp.GetValue("Initial Pressure"); in input_fform()
123 ctrlvar.evis_ini = inp.GetValue("Initial Scalar 1"); in input_fform()
130 ductvari.isetInitial_Duct=(int)inp.GetValue("Set Initial Condition for Duct"); in input_fform()
132 ductvari.isetInlet_Duct=(int)inp.GetValue("Set Inlet Condition for Duct"); in input_fform()
135 n_tmp = (int) inp.GetValue("Number of Blower Surfaces"); //BC_setNBlower(&n_tmp); in input_fform()
144 *ivec[0] = inp.GetValue("Blower Mode"); in input_fform()
145 *ivec[1] = inp.GetValue("Blower Surface ID"); in input_fform()
146 *ivec[2] = inp.GetValue("Blower Enable"); in input_fform()
148 *dvec[0] = inp.GetValue("Blower Cycle Period"); in input_fform()
149 *dvec[1] = inp.GetValue("Blower Full On Period"); in input_fform()
150 *dvec[2] = inp.GetValue("Blower Rise Time"); in input_fform()
151 *dvec[3] = inp.GetValue("Blower Fall Time"); in input_fform()
152 *dvec[4] = inp.GetValue("Blower Maximum u_normal"); in input_fform()
153 *dvec[5] = inp.GetValue("Blower Minimum u_normal"); in input_fform()
154 *dvec[6] = inp.GetValue("Blower Temperature"); in input_fform()
155 *dvec[7] = inp.GetValue("Blower Eddy Viscosity"); in input_fform()
156 *dvec[8] = inp.GetValue("Blower BL Thickness"); in input_fform()
157 *dvec[9] = inp.GetValue("Blower BL Thickness (scalar)"); in input_fform()
177 …ductvari.isetSuctionID_Duct=(int)inp.GetValue("Duct Set Suction Surface ID"); //suction pat… in input_fform()
179 ductvari.suctionVbottom = inp.GetValue("Duct Bottom Suction Normal Velocity"); in input_fform()
180 ductvari.suctionVside_lower = inp.GetValue("Duct Lower Side Suction Normal Velocity"); in input_fform()
181 ductvari.suctionVside_upper = inp.GetValue("Duct Upper Side Surface Normal Velocity"); in input_fform()
182 ductvari.suctionVtop = inp.GetValue("Duct Top Surface Normal Velocity"); in input_fform()
186 ductvari.iDuctgeometryType = (int)inp.GetValue("Duct Geometry Type"); in input_fform()
193 conpar.iALE = inp.GetValue("iALE"); in input_fform()
194 conpar.icoord = inp.GetValue("icoord"); in input_fform()
195 conpar.irs = inp.GetValue("irs"); in input_fform()
196 conpar.iexec = inp.GetValue("iexec"); in input_fform()
197 timpar.ntseq = inp.GetValue("ntseq"); in input_fform()
198 solpar.imap = inp.GetValue("imap"); in input_fform()
203 if((string)inp.GetValue("Equation of State") == "Incompressible") matdat.matflg[0][0] =-1 ; in input_fform()
204 if((string)inp.GetValue("Equation of State") == "Compressible") matdat.matflg[0][0] =0; in input_fform()
205 inpdat.Delt[0] = inp.GetValue("Time Step Size"); in input_fform()
206 inpdat.nstep[0] = inp.GetValue("Number of Timesteps"); in input_fform()
207 if((string)inp.GetValue("Viscous Control")=="Viscous") conpar.navier=1 ; else conpar.navier=0; in input_fform()
209 if ((string)inp.GetValue("Turbulence Model") == "No-Model" ) { in input_fform()
212 } else if ((string)inp.GetValue("Turbulence Model") == "LES" ) { in input_fform()
215 } else if ((string)inp.GetValue("Turbulence Model") == "RANS-SA" ) { in input_fform()
218 } else if ((string)inp.GetValue("Turbulence Model") == "RANS" ) { in input_fform()
221 } else if ((string)inp.GetValue("Turbulence Model") == "RANS-KE" ) { in input_fform()
224 } else if ((string)inp.GetValue("Turbulence Model") == "DES97" ) { in input_fform()
227 } else if ((string)inp.GetValue("Turbulence Model") == "DDES" ) { in input_fform()
241 turbvar.DES_SA_hmin=(double)inp.GetValue("DES SA Minimum Edge Length"); in input_fform()
244 ((string)inp.GetValue("Solve Flow") == "True")? solflow=1:solflow=0; in input_fform()
245 ((string)inp.GetValue("Solve Heat") == "True")? solheat=1:solheat=0; in input_fform()
247 if((string)inp.GetValue("Equation of State") == "Compressible") solheat=0; in input_fform()
248 ilset = (int)inp.GetValue("Solve Level Set"); in input_fform()
249 solscalr = (int)inp.GetValue("Solve Scalars"); in input_fform()
262 levlset.epsilon_ls = inp.GetValue("Number of Elements Across Interface"); in input_fform()
263 levlset.epsilon_lsd = inp.GetValue("Number of Elements Across Interface for Redistancing"); in input_fform()
264 levlset.dtlset = inp.GetValue("Pseudo Time step for Redistancing"); in input_fform()
265 levlset.iExpLSSclr2 = inp.GetValue("Explicit Solve for Redistance Field"); in input_fform()
266 levlset.iExpLSSclr1 = inp.GetValue("Explicit Solve for Scalar 1 Field"); in input_fform()
267 if ((string)inp.GetValue("Apply Volume Constraint") == "True" ) { in input_fform()
269 else if((string)inp.GetValue("Apply Volume Constraint") == "False" ) { in input_fform()
282 conpar.necho = inp.GetValue("Verbosity Level"); in input_fform()
283 outpar.ntout = inp.GetValue("Number of Timesteps between Restarts"); in input_fform()
284 outpar.nsynciofiles = inp.GetValue("Number of SyncIO Files"); in input_fform()
285 if((string)inp.GetValue("Print Statistics") == "True") outpar.ioform = 2; in input_fform()
288 if((string)inp.GetValue("Print Wall Fluxes") == "True") outpar.iowflux = 1; in input_fform()
291 if((string)inp.GetValue("Print FieldView") == "True") outpar.iofieldv = 1; in input_fform()
294 if((string)inp.GetValue("Print ybar") == "True") outpar.ioybar = 1; in input_fform()
297 if((string)inp.GetValue("Print vorticity") == "True") outpar.ivort = 1; in input_fform()
300 outpar.nstepsincycle = inp.GetValue("Number of Steps in a Cycle"); in input_fform()
301 outpar.nphasesincycle = inp.GetValue("Number of Phases in a Cycle"); in input_fform()
302 … outpar.ncycles_startphaseavg = inp.GetValue("Number of Initial Cycles to Skip in Phase Average"); in input_fform()
304 strcpy( outpar.iotype , ((string)inp.GetValue("Data Block Format")).c_str()); in input_fform()
305 strcpy( phasta_iotype , ((string)inp.GetValue("Data Block Format")).c_str()); in input_fform()
306 SONFATH = inp.GetValue("Number of Father Nodes"); in input_fform()
308 if((string)inp.GetValue("Print Residual at End of Step") == "True") genpar.lstres = 1; in input_fform()
311 if((string)inp.GetValue("Print Error Indicators") == "True") turbvar.ierrcalc = 1; in input_fform()
314 if((string)inp.GetValue("Print Velocity Hessian") == "True") turbvar.ihessian = 1; in input_fform()
318 turbvari.ierrsmooth = inp.GetValue("Number of Error Smoothing Iterations"); in input_fform()
321 int nsrfCM = inp.GetValue("Number of Force Surfaces"); in input_fform()
323 vector<int> ivec = inp.GetValue("Surface ID's for Force Calculation"); in input_fform()
331 aerfrc.isrfIM = inp.GetValue("Surface ID for Integrated Mass"); in input_fform()
333 outpar.iv_rankpercore = inp.GetValue("Ranks per core"); in input_fform()
334 outpar.iv_corepernode = inp.GetValue("Cores per node"); in input_fform()
337 if((string)inp.GetValue("Ramp Inflow") == "True") turbvari.iramp=1; in input_fform()
339 vec = inp.GetValue("Mdot Ramp Inflow Start and Stop"); in input_fform()
343 vec = inp.GetValue("Mdot Ramp Lower FC Start and Stop"); in input_fform()
347 vec = inp.GetValue("Mdot Ramp Upper FC Start and Stop"); in input_fform()
354 vec = inp.GetValue("Limit u1"); in input_fform()
360 vec = inp.GetValue("Limit u2"); in input_fform()
366 vec = inp.GetValue("Limit u3"); in input_fform()
372 vec = inp.GetValue("Limit Pressure"); in input_fform()
378 vec = inp.GetValue("Limit Temperature"); in input_fform()
386 if((string)inp.GetValue("Shear Law") == "Constant Viscosity") in input_fform()
389 if((string)inp.GetValue("Bulk Viscosity Law") == "Constant Bulk Viscosity") in input_fform()
392 mmatpar.pr = inp.GetValue("Prandtl Number"); in input_fform()
394 if((string)inp.GetValue("Conductivity Law") == "Constant Conductivity") in input_fform()
397 vec = inp.GetValue("Density"); in input_fform()
403 vec = inp.GetValue("Viscosity"); in input_fform()
415 vec = inp.GetValue("Thermal Conductivity"); in input_fform()
421 vec = inp.GetValue("Scalar Diffusivity"); in input_fform()
427 if((string)inp.GetValue("Zero Mean Pressure") == "True") in input_fform()
430 turbvar.rmutarget = inp.GetValue("Target Viscosity For Step NSTEP"); in input_fform()
432 if ( (string)inp.GetValue("Body Force Option") == "None" ) { in input_fform()
435 else if ( (string)inp.GetValue("Body Force Option") == "Vector" ) { in input_fform()
438 else if ( (string)inp.GetValue("Body Force Option") == "User e3source.f" ) { in input_fform()
441 else if ( (string)inp.GetValue("Body Force Option") == "Boussinesq" ) { in input_fform()
444 else if ( (string)inp.GetValue("Body Force Option") == "Cooling Analytic" ) { in input_fform()
446 ctrlvar.xvel_ini = inp.GetValue("Initial X Velocity"); in input_fform()
447 ctrlvar.yvel_ini = inp.GetValue("Initial Y Velocity"); in input_fform()
448 ctrlvar.zvel_ini = inp.GetValue("Initial Z Velocity"); in input_fform()
449 ctrlvar.temp_ini = inp.GetValue("Initial Temp"); in input_fform()
450 ctrlvar.pres_ini = inp.GetValue("Initial Pressure"); in input_fform()
452 else if ( (string)inp.GetValue("Body Force Option") == "Cooling Initial Condition" ) { in input_fform()
460 spongevar.betamax = inp.GetValue("Maximum Value of Sponge Parameter"); in input_fform()
461 spongevar.zinsponge = inp.GetValue("Inflow Cooling Sponge Ends at z"); in input_fform()
462 spongevar.zoutsponge= inp.GetValue("Outflow Cooling Sponge Begins at z"); in input_fform()
463 spongevar.radsponge = inp.GetValue("Radial Cooling Sponge Begins at r"); in input_fform()
464 spongevar.grthosponge = inp.GetValue("Sponge Growth Coefficient Outflow"); in input_fform()
465 spongevar.grthisponge = inp.GetValue("Sponge Growth Coefficient Inflow"); in input_fform()
474 if((string)inp.GetValue("Sponge for Continuity Equation") == "True") in input_fform()
476 if((string)inp.GetValue("Sponge for x Momentum Equation") == "True") in input_fform()
478 if((string)inp.GetValue("Sponge for y Momentum Equation") == "True") in input_fform()
480 if((string)inp.GetValue("Sponge for z Momentum Equation") == "True") in input_fform()
482 if((string)inp.GetValue("Sponge for Energy Equation") == "True") in input_fform()
487 vec = inp.GetValue("Body Force"); in input_fform()
495 vec = inp.GetValue("Body Force Pressure Gradient"); in input_fform()
503 if ( (string)inp.GetValue("Surface Tension Option") == "No" ){ in input_fform()
506 else if ((string)inp.GetValue("Surface Tension Option") == "Yes" ){ in input_fform()
515 genpar.Bo = inp.GetValue("Bond Number"); in input_fform()
518 genpar.EntropyPressure = inp.GetValue("Entropy Form of Pressure Constraint on Weight Space"); in input_fform()
521 if ( (string)inp.GetValue("Rotating Frame of Reference") == "True" ) { in input_fform()
523 vec = inp.GetValue("Rotating Frame of Reference Rotation Rate"); in input_fform()
541 if( (string)inp.GetValue("Solver Type") =="svLS" ){ in input_fform()
543 if( (string)inp.GetValue("Solver Type") =="ACUSIM with P Projection" ){ in input_fform()
545 else if ( (string)inp.GetValue("Solver Type") =="ACUSIM" ){ in input_fform()
547 else if( (string)inp.GetValue("Solver Type") =="ACUSIM with Velocity Projection" ){ in input_fform()
549 else if( (string)inp.GetValue("Solver Type") =="ACUSIM with Full Projection" ){ in input_fform()
551 else if( (string)inp.GetValue("Solver Type") =="GMRES Matrix Free"){ in input_fform()
553 else if( (string)inp.GetValue("Solver Type") =="GMRES EBE"){ in input_fform()
555 else if( (string)inp.GetValue("Solver Type") =="PETSc"){ in input_fform()
562 solpar.nGMRES = inp.GetValue("Number of GMRES Sweeps per Solve"); in input_fform()
563 solpar.Kspace = inp.GetValue("Number of Krylov Vectors per GMRES Sweep"); in input_fform()
564 inpdat.LHSupd[0] = inp.GetValue("Number of Solves per Left-hand-side Formation"); in input_fform()
565 inpdat.epstol[0] = inp.GetValue("Tolerance on Momentum Equations"); in input_fform()
566 incomp.prestol = inp.GetValue("Tolerance on ACUSIM Pressure Projection"); in input_fform()
567 incomp.minIters = inp.GetValue("Minimum Number of Iterations per Nonlinear Iteration"); in input_fform()
568 incomp.maxIters = inp.GetValue("Maximum Number of Iterations per Nonlinear Iteration"); in input_fform()
569 inpdat.deltol[0][0]=inp.GetValue("Velocity Delta Ratio"); in input_fform()
570 inpdat.deltol[1][0]=inp.GetValue("Pressure Delta Ratio"); in input_fform()
571 incomp.nPrjs = inp.GetValue("Number of Velocity Projection Vectors"); in input_fform()
572 incomp.nPresPrjs = inp.GetValue("Number of Pressure Projection Vectors"); in input_fform()
573 incomp.iverbose = inp.GetValue("ACUSIM Verbosity Level"); in input_fform()
576 inpdat.epstol[1]=inp.GetValue("Temperature Solver Tolerance"); in input_fform()
577 inpdat.LHSupd[1]=inp.GetValue("Number of Solves of Temperature per Left-hand-side Formation"); in input_fform()
587 inpdat.epstol[2]=inp.GetValue("Scalar 1 Solver Tolerance"); in input_fform()
588 inpdat.LHSupd[2]=inp.GetValue("Number of Solves of Scalar 1 per Left-hand-side Formation"); in input_fform()
590 vec = inp.GetValue("Limit Scalar 1"); in input_fform()
598 inpdat.epstol[3]=inp.GetValue("Scalar 2 Solver Tolerance"); in input_fform()
599 inpdat.LHSupd[3]=inp.GetValue("Number of Solves of Scalar 2 per Left-hand-side Formation"); in input_fform()
601 vec = inp.GetValue("Limit Scalar 2"); in input_fform()
609 inpdat.epstol[4]=inp.GetValue("Scalar 3 Solver Tolerance"); in input_fform()
610 inpdat.LHSupd[4]=inp.GetValue("Number of Solves of Scalar 3 per Left-hand-side Formation"); in input_fform()
612 vec = inp.GetValue("Limit Scalar 3"); in input_fform()
620 inpdat.epstol[5]=inp.GetValue("Scalar 4 Solver Tolerance"); in input_fform()
621 inpdat.LHSupd[5]=inp.GetValue("Number of Solves of Scalar 4 per Left-hand-side Formation"); in input_fform()
623 vec = inp.GetValue("Limit Scalar 4"); in input_fform()
632 genpar.ipord = inp.GetValue("Basis Function Order"); in input_fform()
633 if((string)inp.GetValue("Time Integration Rule") == "First Order") in input_fform()
635 else inpdat.rhoinf[0] = (double)inp.GetValue("Time Integration Rho Infinity"); in input_fform()
636 if((string)inp.GetValue("Predictor at Start of Step")=="Same Velocity") in input_fform()
638 if((string)inp.GetValue("Predictor at Start of Step")=="Zero Acceleration") in input_fform()
640 if((string)inp.GetValue("Predictor at Start of Step")=="Same Acceleration") in input_fform()
642 if((string)inp.GetValue("Predictor at Start of Step")=="Same Delta") in input_fform()
645 if((string)inp.GetValue("Weak Form") == "Galerkin") in input_fform()
647 if((string)inp.GetValue("Weak Form") == "SUPG") in input_fform()
650 if((string)inp.GetValue("Flow Advection Form") == "Convective") in input_fform()
652 else if((string)inp.GetValue("Flow Advection Form") == "Conservative") in input_fform()
654 if((string)inp.GetValue("Scalar Advection Form") == "Convective") in input_fform()
656 else if((string)inp.GetValue("Scalar Advection Form") == "Conservative") in input_fform()
658 if((string)inp.GetValue("Use Conservative Scalar Convection Velocity") == "True") in input_fform()
660 else if((string)inp.GetValue("Use Conservative Scalar Convection Velocity") == "False") in input_fform()
663 if((string)inp.GetValue("Tau Matrix") == "Diagonal-Shakib") in input_fform()
665 else if((string)inp.GetValue("Tau Matrix") == "Diagonal-Franca") in input_fform()
667 else if((string)inp.GetValue("Tau Matrix") == "Diagonal-Jansen(dev)") in input_fform()
669 else if((string)inp.GetValue("Tau Matrix") == "Diagonal-Compressible") in input_fform()
671 else if((string)inp.GetValue("Tau Matrix") == "Matrix-Mallet") in input_fform()
673 else if((string)inp.GetValue("Tau Matrix") == "Matrix-Modal") in input_fform()
676 genpar.dtsfct = inp.GetValue("Tau Time Constant"); in input_fform()
677 genpar.taucfct = inp.GetValue("Tau C Scale Factor"); in input_fform()
679 genpar.iLHScond = inp.GetValue("LHS BC heat flux enable"); in input_fform()
683 if((string)inp.GetValue("Discontinuity Capturing") == "Off") solpar.iDC = 0; in input_fform()
684 else if((string)inp.GetValue("Discontinuity Capturing") == "DC-mallet") solpar.iDC = 1; in input_fform()
685 else if((string)inp.GetValue("Discontinuity Capturing") == "DC-quadratic") solpar.iDC = 2; in input_fform()
686 else if((string)inp.GetValue("Discontinuity Capturing") == "DC-minimum") solpar.iDC = 3; in input_fform()
694 vector<int> ivec = inp.GetValue("Scalar Discontinuity Capturing"); in input_fform()
706 if((string)inp.GetValue("Include Viscous Correction in Stabilization") == "True") in input_fform()
714 genpar.irampViscOutlet = (int)inp.GetValue("Ramp Up Viscosity Near Outlet"); in input_fform()
716 genpar.istretchOutlet = (int)inp.GetValue("Stretch X Coordinate Near Outlet"); in input_fform()
719 genpar.iremoveStabTimeTerm = (int)inp.GetValue("Remove Time Term from Stabilization"); in input_fform()
721 timdat.flmpl = inp.GetValue("Lumped Mass Fraction on Left-hand-side"); in input_fform()
722 timdat.flmpr = inp.GetValue("Lumped Mass Fraction on Right-hand-side"); in input_fform()
725 if((string)inp.GetValue("Dump CFL") == "True") in input_fform()
728 intdat.intg[0][0]=inp.GetValue("Quadrature Rule on Interior"); in input_fform()
729 intdat.intg[0][1]=inp.GetValue("Quadrature Rule on Boundary"); in input_fform()
730 genpar.ibksiz = inp.GetValue("Number of Elements Per Block"); in input_fform()
732 ((string)inp.GetValue("Turn Off Source Terms for Scalars") in input_fform()
734 sclrs.tdecay=inp.GetValue("Decay Multiplier for Scalars"); in input_fform()
742 turbvari.nohomog =inp.GetValue("Number of Homogenous Directions"); in input_fform()
744 if((string)inp.GetValue("Turbulence Wall Model Type") == "Slip Velocity") turbvar.itwmod = 1; in input_fform()
745 …else if((string)inp.GetValue("Turbulence Wall Model Type") == "Effective Viscosity") turbvar.itwmo… in input_fform()
748 ifrule = inp.GetValue("Velocity Averaging Steps"); in input_fform()
753 if((string)inp.GetValue("Dynamic Model Type") == "Bardina") turbvari.iles += 10; in input_fform()
754 else if((string)inp.GetValue("Dynamic Model Type") == "Projection") turbvari.iles += 20; in input_fform()
756 ifrule = inp.GetValue("Filter Integration Rule"); in input_fform()
758 ifrule = inp.GetValue("Dynamic Model Averaging Steps"); in input_fform()
760 turbvar.fwr1 = inp.GetValue("Filter Width Ratio"); in input_fform()
761 turbvar.flump = inp.GetValue("Lumping Factor for Filter"); in input_fform()
764 if ((string)inp.GetValue("Model Statistics") == "True" ) { in input_fform()
769 if ((string)inp.GetValue("Double Filter") == "True" ) { in input_fform()
774 if ((string)inp.GetValue("Model/SUPG Dissipation") == "True" ) { in input_fform()
780 if((string)inp.GetValue("Dynamic Model Type") == "Standard") { in input_fform()
782 if((string)inp.GetValue("Dynamic Sub-Model Type") == "None") in input_fform()
784 else if((string)inp.GetValue("Dynamic Sub-Model Type") =="DFWR") in input_fform()
786 else if((string)inp.GetValue("Dynamic Sub-Model Type") =="SUPG") in input_fform()
789 else if((string)inp.GetValue("Dynamic Model Type") == "Projection") { in input_fform()
791 if((string)inp.GetValue("Projection Filter Type") == "Linear") in input_fform()
793 else if((string)inp.GetValue("Projection Filter Type") =="Quadratic") in input_fform()
796 if((string)inp.GetValue("Dynamic Sub-Model Type") == "None") in input_fform()
798 else if((string)inp.GetValue("Dynamic Sub-Model Type") =="ConsistentProj") in input_fform()
807 if ( (spebcvr.irscale = inp.GetValue("SPEBC Model Active")) >= 0 ){ in input_fform()
809 ifrule = inp.GetValue("Velocity Averaging Steps"); in input_fform()
811 spebcvr.intpres = inp.GetValue("Interpolate Pressure"); in input_fform()
812 spebcvr.plandist = inp.GetValue("Distance between Planes"); in input_fform()
813 spebcvr.thetag = inp.GetValue("Theta Angle of Arc"); in input_fform()
814 spebcvr.ds = inp.GetValue("Distance for Velocity Averaging"); in input_fform()
815 spebcvr.tolerence = inp.GetValue("SPEBC Cylindrical Tolerance"); in input_fform()
816 spebcvr.radcyl = inp.GetValue("Radius of recycle plane"); in input_fform()
817 spebcvr.rbltin = inp.GetValue("Inlet Boundary Layer Thickness"); in input_fform()
818 spebcvr.rvscal = inp.GetValue("Vertical Velocity Scale Factor"); in input_fform()
822 if ( (string)inp.GetValue("Time Varying Boundary Conditions From File") == "True") in input_fform()
828 nomodule.bcttimescale = inp.GetValue("BCT Time Scale Factor"); in input_fform()
831 if( (nomodule.icardio = inp.GetValue("Number of Coupled Surfaces")) ){ in input_fform()
836 if ( (string)inp.GetValue("Pressure Coupling") == "None") in input_fform()
838 if ( (string)inp.GetValue("Pressure Coupling") == "Explicit") in input_fform()
840 if ( (string)inp.GetValue("Pressure Coupling") == "Implicit") in input_fform()
842 if ( (string)inp.GetValue("Pressure Coupling") == "P-Implicit") in input_fform()
845 if( (nomodule.numResistSrfs=inp.GetValue("Number of Resistance Surfaces")) ){ in input_fform()
846 ivec = inp.GetValue("List of Resistance Surfaces"); in input_fform()
851 vec = inp.GetValue("Resistance Values"); in input_fform()
856 if( (nomodule.numImpSrfs=inp.GetValue("Number of Impedance Surfaces")) ){ in input_fform()
857 ivec = inp.GetValue("List of Impedance Surfaces"); in input_fform()
862 if ( (string)inp.GetValue("Impedance From File") == "True") in input_fform()
865 if( (nomodule.numRCRSrfs=inp.GetValue("Number of RCR Surfaces")) ){ in input_fform()
866 ivec = inp.GetValue("List of RCR Surfaces"); in input_fform()
871 if ( (string)inp.GetValue("RCR Values From File") == "True") in input_fform()
876 if((string)inp.GetValue("Deformable Wall")=="True"){ in input_fform()
878 nomodule.rhovw = inp.GetValue("Density of Vessel Wall"); in input_fform()
879 nomodule.thicknessvw = inp.GetValue("Thickness of Vessel Wall"); in input_fform()
880 nomodule.evw = inp.GetValue("Young Mod of Vessel Wall"); in input_fform()
881 nomodule.rnuvw = inp.GetValue("Poisson Ratio of Vessel Wall"); in input_fform()
882 nomodule.rshearconstantvw = inp.GetValue("Shear Constant of Vessel Wall"); in input_fform()
883 if((string)inp.GetValue("Wall Mass Matrix for LHS") == "True") nomodule.iwallmassfactor = 1; in input_fform()
885 … if((string)inp.GetValue("Wall Stiffness Matrix for LHS") == "True") nomodule.iwallstiffactor = 1; in input_fform()
889 if((string)inp.GetValue("Viscous Flux Flag") == "True") nomodule.iviscflux = 1; in input_fform()
890 if((string)inp.GetValue("Viscous Flux Flag") == "False") nomodule.iviscflux = 0; in input_fform()
895 outpar.ro = inp.GetValue("Density"); in input_fform()
896 outpar.vel = inp.GetValue("Velocity"); in input_fform()
897 outpar.press = inp.GetValue("Pressure"); in input_fform()
898 outpar.temper = inp.GetValue("Temperature"); in input_fform()
899 outpar.entrop = inp.GetValue("Entropy"); in input_fform()
904 ivec = inp.GetValue("Step Construction"); in input_fform()