pyNastran  0.5.0
pyNastran BDF Reader/Writer, OP2 Parser, and GUI
Class List
Here are the classes, structs, unions and interfaces with brief descriptions:
pyNastran.bdf.cards.sets.ABCQSetGeneric Class ASET, BSET, CSET, QSET cards inherit from
pyNastran.bdf.cards.sets.ABQSet1Generic Class ASET1, BSET1, QSET1 cards inherit from
pyNastran.bdf.cards.loads.staticLoads.ACCEL1Acceleration Load Defines static acceleration loads at individual GRID points
pyNastran.op2.tables.oug.oug_accelerations.AccelerationObject
pyNastran.bdf.bdfInterface.addCard.AddMethods
pyNastran.bdf.cards.aero.AEFACTDefines real numbers for aeroelastic analysis
pyNastran.bdf.cards.aero.AELINKDefines relationships between or among AESTAT and AESURF entries, such that:

\[ u^D + \Sigma_{i=1}^n C_i u_i^I = 0.0\]

AELINK ID LABLD LABL1 C1 LABL2 C2 LABL3 C3 LABL4 C4 -etc

pyNastran.bdf.cards.aero.AELISTDefines a list of aerodynamic elements to undergo the motion prescribed with the AESURF Bulk Data entry for static aeroelasticity
pyNastran.bdf.cards.aero.AEPARMDefines a general aerodynamic trim variable degree-of-freedom (aerodynamic extra point)
pyNastran.bdf.cards.aero.AeroBase class for AERO and AEROS cards
pyNastran.bdf.cards.aero.AEROGives basic aerodynamic parameters for unsteady aerodynamics
pyNastran.bdf.cards.aero.AEROSGives basic aerodynamic parameters for unsteady aerodynamics
pyNastran.bdf.cards.aero.AESTATSpecifies rigid body motions to be used as trim variables in static aeroelasticity
pyNastran.bdf.cards.aero.AESURFSpecifies an aerodynamic control surface as a member of the set of aerodynamic extra points
pyNastran.bdf.cards.aero.AESURFSOptional specification of the structural nodes associated with an aerodynamic control surface that has been defined on an AESURF entry
pyNastran.all_tests.AllTests
pyNastran.bdf.cards.materials.AnisotropicMaterialAnisotropic Material Class
pyNastran.gui.gui.AppFrame
pyNastran.op2.tables.opg_appliedLoads.opg_Objects.AppliedLoadsObject
pyNastran.bdf.cards.sets.ASETDefines degrees-of-freedom in the analysis set (a-set)
pyNastran.bdf.cards.sets.ASET1Defines degrees-of-freedom in the analysis set (a-set) ASET1 C ID1 ID2 ID3 ID4 ID5 ID6 ID7 ID8 ID9 ASET1 C ID1 'THRU' ID2
pyNastran.op2.tables.oes_stressStrain.real.oes_bars.BarStrainObject# sCode=10 S T R A I N S I N B A R E L E M E N T S ( C B A R ) ELEMENT SA1 SA2 SA3 SA4 AXIAL SA-MAX SA-MIN M.S
pyNastran.op2.tables.oes_stressStrain.real.oes_bars.BarStressObject# sCode=0 S T R E S S E S I N B A R E L E M E N T S ( C B A R ) ELEMENT SA1 SA2 SA3 SA4 AXIAL SA-MAX SA-MIN M.S
pyNastran.bdf.cards.baseCard.BaseCard
pyNastran.op2.resultObjects.op2_Objects.baseScalarObject
pyNastran.bdf.bdf.BDFNASTRAN BDF Reader/Writer/Editor class
pyNastran.bdf.bdfInterface.BDF_Card.BDFCard
pyNastran.bdf.bdf_Methods.BDFMethods
pyNastran.bdf.bdfInterface.bdf_Reader.BDFReader
pyNastran.op2.tables.oes_stressStrain.real.oes_beams.BeamStrainObject
pyNastran.op2.tables.oes_stressStrain.real.oes_beams.BeamStressObject[1,0,0] S T R E S S E S I N B E A M E L E M E N T S ( C B E A M ) STAT DIST/ ELEMENT-ID GRID LENGTH SXC SXD SXE SXF S-MAX S-MIN M.S
pyNastran.bdf.cards.sets.BSETDefines analysis set (a-set) degrees-of-freedom to be fixed (b-set) during generalized dynamic reduction or component mode synthesis calculations
pyNastran.bdf.cards.sets.BSET1
pyNastran.bdf.cards.elements.bush.BushElement
pyNastran.bdf.cards.properties.bush.BushingProperty
pyNastran.bdf.cards.aero.CAERO1Defines an aerodynamic macro element (panel) in terms of two leading edge locations and side chords
pyNastran.bdf.cards.aero.CAERO2Aerodynamic Body Connection Defines aerodynamic slender body and interference elements for Doublet-Lattice aerodynamics
pyNastran.bdf.cards.aero.CAERO3
pyNastran.bdf.cards.aero.CAERO4
pyNastran.bdf.cards.aero.CAERO5
pyNastran.bdf.errors.CardInstantiationError
pyNastran.bdf.bdfInterface.bdf_cardMethods.CardMethods
pyNastran::bdf::errors::CardParseErrorGNU Lesser General Public License
pyNastran.converters.cart3d.cart3d_reader.Cart3DAsciiReader
pyNastran.converters.cart3d.cart3d_reader.Cart3DBinaryReader
pyNastran.converters.cart3d.cart3dIO.Cart3dIO
pyNastran.converters.cart3d.toPanair.Cart3dToPanair
pyNastran.bdf.caseControlDeck.CaseControlDeck
pyNastran.bdf.cards.elements.bars.CBARCBAR EID PID GA GB X1 X2 X3 OFFT PA PB W1A W2A W3A W1B W2B W3B or CBAR EID PID GA GB G0 OFFT PA PB W1A W2A W3A W1B W2B W3B
pyNastran.bdf.cards.elements.bars.CBEAMCBEAM EID PID GA GB X1 X2 X3 OFFT/BIT PA PB W1A W2A W3A W1B W2B W3B SA SB or CBEAM EID PID GA GB G0 - - OFFT/BIT PA PB W1A W2A W3A W1B W2B W3B SA SB
pyNastran.bdf.cards.elements.bars.CBEAM3Defines a three-node beam element
pyNastran.bdf.cards.elements.bars.CBEND
pyNastran.bdf.cards.elements.bush.CBUSH
pyNastran.bdf.cards.elements.bush.CBUSH1D
pyNastran.bdf.cards.elements.bush.CBUSH2D2-D Linear-Nonlinear Connection Defines the connectivity of a two-dimensional Linear-Nonlinear element
pyNastran.bdf.cards.elements.damper.CDAMP1
pyNastran.bdf.cards.elements.damper.CDAMP2
pyNastran.bdf.cards.elements.damper.CDAMP3
pyNastran.bdf.cards.elements.damper.CDAMP4
pyNastran.bdf.cards.elements.damper.CDAMP5
pyNastran.bdf.cards.elements.springs.CELAS1
pyNastran.bdf.cards.elements.springs.CELAS2
pyNastran.bdf.cards.elements.springs.CELAS3
pyNastran.bdf.cards.elements.springs.CELAS4
pyNastran.op2.tables.oes_stressStrain.real.oes_springs.CelasStrainObject
pyNastran.op2.tables.oes_stressStrain.real.oes_springs.CelasStressObjectS T R E S S E S I N S C A L A R S P R I N G S ( C E L A S 2 ) TIME STRESS TIME STRESS TIME STRESS TIME STRESS 0.0 0.0 5.000000E-02 0.0 1.000000E-01 0.0 1.500000E-01 0.0 2.000000E-01 0.0 2.500000E-01 0.0 3.000000E-01 0.0 3.500000E-01 0.0
pyNastran.bdf.cards.elements.elements.CFAST
pyNastran.bdf.cards.elements.elements.CGAP
pyNastran.bdf.cards.thermal.thermal.CHBDYEDefines a boundary condition surface element with reference to a heat conduction element
pyNastran.bdf.cards.thermal.thermal.CHBDYGDefines a boundary condition surface element without reference to a property entry
pyNastran.bdf.cards.thermal.thermal.CHBDYPDefines a boundary condition surface element with reference to a PHBDY entry
pyNastran.bdf.cards.elements.solid.CHEXA20CHEXA EID PID G1 G2 G3 G4 G5 G6 G7 G8 G9 G10 G11 G12 G13 G14 G15 G16 G17 G18 G19 G20
pyNastran.bdf.cards.elements.solid.CHEXA8CHEXA EID PID G1 G2 G3 G4 G5 G6 G7 G8
pyNastran.bdf.cards.elements.mass.CMASS1Defines a scalar mass element
pyNastran.bdf.cards.elements.mass.CMASS2Defines a scalar mass element without reference to a property entry
pyNastran.bdf.cards.elements.mass.CMASS3Defines a scalar mass element that is connected only to scalar points
pyNastran.bdf.cards.elements.mass.CMASS4Defines a scalar mass element that is connected only to scalar points, without reference to a property entry CMASS4 EID M S1 S2
pyNastran.op2.tables.oug.oug_accelerations.ComplexAccelerationObject
pyNastran.op2.tables.oes_stressStrain.complex.oes_bars.ComplexBarStrainObject# sCode=10 S T R A I N S I N B A R E L E M E N T S ( C B A R ) ELEMENT SA1 SA2 SA3 SA4 AXIAL SA-MAX SA-MIN M.S
pyNastran.op2.tables.oes_stressStrain.complex.oes_bars.ComplexBarStressObject# sCode=0 C O M P L E X S T R E S S E S I N B A R E L E M E N T S ( C B A R ) (MAGNITUDE/PHASE)
pyNastran.op2.tables.oef_forces.oef_complexForceObjects.ComplexBendForce
pyNastran.op2.tables.oef_forces.oef_complexForceObjects.ComplexCBARForce
pyNastran.op2.tables.oef_forces.oef_complexForceObjects.ComplexCBeamForce
pyNastran.op2.tables.oef_forces.oef_complexForceObjects.ComplexCBUSHForce
pyNastran.op2.tables.oes_stressStrain.complex.oes_springs.ComplexCelasStrainObject
pyNastran.op2.tables.oes_stressStrain.complex.oes_springs.ComplexCelasStressObjectS T R E S S E S I N S C A L A R S P R I N G S ( C E L A S 2 ) TIME STRESS TIME STRESS TIME STRESS TIME STRESS 0.0 0.0 5.000000E-02 0.0 1.000000E-01 0.0 1.500000E-01 0.0 2.000000E-01 0.0 2.500000E-01 0.0 3.000000E-01 0.0 3.500000E-01 0.0
pyNastran.op2.tables.oef_forces.oef_complexForceObjects.ComplexCShearForce
pyNastran.op2.tables.oef_forces.oef_complexForceObjects.ComplexDamperForce
pyNastran.op2.tables.oug.oug_displacements.ComplexDisplacementObject
pyNastran.op2.tables.lama_eigenvalues.lama_objects.ComplexEigenvalues
pyNastran.op2.tables.oug.oug_eigenvectors.ComplexEigenVectorObject
pyNastran.op2.tables.oes_stressStrain.complex.elementsStressStrain.ComplexElementsStressStrain
pyNastran.op2.tables.oef_forces.oef_complexForceObjects.ComplexForce_VU
pyNastran.op2.tables.oef_forces.oef_complexForceObjects.ComplexForce_VU_2D
pyNastran.op2.tables.oef_forces.complexForces.ComplexForces
pyNastran.op2.tables.opg_appliedLoads.opnl_forceVector.ComplexForceVectorObject
pyNastran.op2.tables.ogf_gridPointForces.ogf_Objects.complexGridPointForcesObject
pyNastran.op2.tables.opg_appliedLoads.opg_loadVector.ComplexLoadVectorObject
pyNastran.op2.tables.oqg_constraintForces.oqg_mpcForces.ComplexMPCForcesObject
pyNastran.op2.tables.oef_forces.oef_complexForceObjects.ComplexPentaPressureForce
pyNastran.op2.tables.oef_forces.oef_complexForceObjects.ComplexPLATE2Force
pyNastran.op2.tables.oef_forces.oef_complexForceObjects.ComplexPlateForce
pyNastran.op2.tables.oes_stressStrain.complex.oes_plates.ComplexPlateStrainObject# ??? - is this just 11 ELEMENT STRAIN STRAINS IN ELEMENT COORD SYSTEM PRINCIPAL STRAINS (ZERO SHEAR) ID
pyNastran.op2.tables.oes_stressStrain.complex.oes_plates.ComplexPlateStressObjectC O M P L E X S T R E S S E S I N Q U A D R I L A T E R A L E L E M E N T S ( Q U A D 8 ) (REAL/IMAGINARY)
pyNastran.op2.tables.oes_stressStrain.complex.oes_rods.ComplexRodDamperObject
pyNastran.op2.tables.oef_forces.oef_complexForceObjects.ComplexRodForce
pyNastran.op2.tables.oes_stressStrain.complex.oes_rods.ComplexRodStrainObject
pyNastran.op2.tables.oes_stressStrain.complex.oes_rods.ComplexRodStressObject
pyNastran.op2.tables.oqg_constraintForces.oqg_spcForces.ComplexSPCForcesObject
pyNastran.op2.tables.oef_forces.oef_complexForceObjects.ComplexSpringForce
pyNastran.op2.resultObjects.tableObject.ComplexTableObject
pyNastran.op2.tables.oug.oug_velocities.ComplexVelocityObject
pyNastran.op2.tables.oef_forces.oef_complexForceObjects.ComplexViscForce
pyNastran.op2.tables.oes_stressStrain.real.oes_compositePlates.CompositePlateStrainObject??? ELEMENT PLY STRESSES IN FIBER AND MATRIX DIRECTIONS INTER-LAMINAR STRESSES PRINCIPAL STRESSES (ZERO SHEAR) MAX ID ID NORMAL-1 NORMAL-2 SHEAR-12 SHEAR XZ-MAT SHEAR YZ-MAT ANGLE MAJOR MINOR SHEAR
pyNastran.op2.tables.oes_stressStrain.real.oes_compositePlates.CompositePlateStressObject# sCode = 0 S T R E S S E S I N L A Y E R E D C O M P O S I T E E L E M E N T S ( Q U A D 4 ) ELEMENT PLY STRESSES IN FIBER AND MATRIX DIRECTIONS INTER-LAMINAR STRESSES PRINCIPAL STRESSES (ZERO SHEAR) MAX ID ID NORMAL-1 NORMAL-2 SHEAR-12 SHEAR XZ-MAT SHEAR YZ-MAT ANGLE MAJOR MINOR SHEAR
pyNastran.bdf.cards.elements.mass.CONM1
pyNastran.bdf.cards.elements.mass.CONM2
pyNastran.bdf.cards.elements.bars.CONROD
pyNastran.bdf.cards.constraints.Constraint
pyNastran.bdf.cards.constraints.ConstraintADD
pyNastran.bdf.cards.constraints.constraintObject
pyNastran.bdf.cards.constraints.constraintObject2
pyNastran.bdf.cards.thermal.thermal.CONVSpecifies a free convection boundary condition for heat transfer analysis through connection to a surface element (CHBDYi entry)
pyNastran.bdf.cards.coordinateSystems.Coord
pyNastran.bdf.cards.coordinateSystems.CORD1C
pyNastran.bdf.cards.coordinateSystems.CORD1R
pyNastran.bdf.cards.coordinateSystems.CORD1S
pyNastran.bdf.cards.coordinateSystems.Cord1x
pyNastran.bdf.cards.coordinateSystems.CORD2C
pyNastran.bdf.cards.coordinateSystems.CORD2R
pyNastran.bdf.cards.coordinateSystems.CORD2S
pyNastran.bdf.cards.coordinateSystems.Cord2x
pyNastran.bdf.cards.coordinateSystems.CORD3GDefines a general coordinate system using three rotational angles as functions of coordinate values in the reference coordinate system
pyNastran.bdf.cards.elements.solid.CPENTA15CPENTA EID PID G1 G2 G3 G4 G5 G6 G7 G8 G9 G10 G11 G12 G13 G14 G15
pyNastran.bdf.cards.elements.solid.CPENTA6CPENTA EID PID G1 G2 G3 G4 G5 G6 *----------* / \ / \ / A \ / c \ *---*-----*-----* V = (A1+A2)/2 * (c1-c2) C = (c1-c2)/2
pyNastran.bdf.cards.elements.shell.CQUAD
pyNastran.bdf.cards.elements.shell.CQUAD4
pyNastran.bdf.cards.elements.shell.CQUAD8
pyNastran.bdf.cards.elements.shell.CQUADR
pyNastran.bdf.cards.elements.shell.CQUADX
pyNastran.bdf.cards.elements.elements.CRAC2D
pyNastran.bdf.cards.elements.elements.CRAC3D
pyNastran.bdf.cards.elements.elements.CrackElement
pyNastran.bdf.cards.properties.properties.CrackProperty
pyNastran.bdf.cards.materials.CREEP
pyNastran.bdf.cards.elements.bars.CROD
pyNastran.bdf.cards.sets.CSETDefines analysis set (a-set) degrees-of-freedom to be fixed (b-set) during generalized dynamic reduction or component mode synthesis calculations
pyNastran.bdf.cards.sets.CSET1Defines analysis set (a-set) degrees-of-freedom to be fixed (b-set) during generalized dynamic reduction or component mode synthesis calculations
pyNastran.bdf.cards.elements.shell.CSHEAR
pyNastran.bdf.cards.aero.CSSCHDDefines a scheduled control surface deflection as a function of Mach number and angle of attack
pyNastran.bdf.cards.elements.solid.CTETRA10CTETRA EID PID G1 G2 G3 G4 G5 G6 G7 G8 G9 G10 CTETRA 1 1 239 229 516 99 335 103 265 334 101 102
pyNastran.bdf.cards.elements.solid.CTETRA4CTETRA EID PID G1 G2 G3 G4
pyNastran.bdf.cards.elements.shell.CTRIA3
pyNastran.bdf.cards.elements.shell.CTRIA6
pyNastran.bdf.cards.elements.shell.CTRIAR
pyNastran.bdf.cards.elements.shell.CTRIAX
pyNastran.bdf.cards.elements.shell.CTRIAX6Nodes defined in a non-standard way 5 / \ 6 4 / \ 1----2----3
pyNastran.bdf.cards.elements.bars.CTUBE
pyNastran.bdf.cards.elements.damper.CVISC
pyNastran.bdf.cards.coordinateSystems.CylindricalCoord

\[ r = \sqrt(x^2+y^2) \]

\[ \theta = tan^-1(\frac{y}{x}) \]

\[ z = z \]

pyNastran.bdf.cards.elements.damper.DamperElement
pyNastran.bdf.cards.properties.damper.DamperProperty
pyNastran.bdf.cards.loads.loads.DAREADefines scale (area) factors for static and dynamic loads
pyNastran.bdf.cards.optimization.DCONSTR
pyNastran.bdf.cards.optimization.DDVAL
pyNastran.general.logger.debugLogger
pyNastran.bdf.cards.dmig.DEQATN
pyNastran.op2.tables.destab.DESTAB
pyNastran.bdf.cards.optimization.DESVAR
pyNastran.op2.tables.oug.oug_displacements.DisplacementObject
pyNastran.op2.tables.geom.dit.DIT
pyNastran.bdf.cards.optimization.DLINK
pyNastran.bdf.cards.loads.loads.DLOAD
pyNastran.bdf.cards.dmig.DMI
pyNastran.bdf.cards.dmig.DMIGDefines direct input matrices related to grid, extra, and/or scalar points
pyNastran.bdf.cards.dmig.DMIJDirect Matrix Input at js-Set of the Aerodynamic Mesh Defines direct input matrices related to collation degrees-of-freedom (js-set) of aerodynamic mesh points for CAERO1, CAERO3, CAERO4 and CAERO5 and for the slender body elements of CAERO2
pyNastran.bdf.cards.dmig.DMIJIDirect Matrix Input at js-Set of the Interference Body Defines direct input matrices related to collation degrees-of-freedom (js-set) of aerodynamic mesh points for the interference elements of CAERO2
pyNastran.bdf.cards.dmig.DMIKDirect Matrix Input at ks-Set of the Aerodynamic Mesh Defines direct input matrices related to physical (displacement) degrees-of-freedom (ks-set) of aerodynamic grid points
pyNastran.bdf.cards.optimization.DOPTPRM
pyNastran.bdf.cards.optimization.DRESP1
pyNastran.bdf.cards.optimization.DRESP2
pyNastran.bdf.cards.optimization.DSCREEN
pyNastran.general.logger.dummyLogger
pyNastran.bdf.cards.optimization.DVMREL1
pyNastran.bdf.cards.optimization.DVPREL1
pyNastran.bdf.cards.optimization.DVPREL2
pyNastran.op2.tables.geom.dynamics.DYNAMICS
pyNastran.bdf.cards.methods.EIGBDefines data needed to perform buckling analysis
pyNastran.bdf.cards.methods.EIGCDefines data needed to perform complex eigenvalue analysis
pyNastran.op2.tables.oug.oug_eigenvectors.EigenVectorObjectEIGENVALUE = 6.158494E+07 CYCLES = 1.248985E+03 R E A L E I G E N V E C T O R N O
pyNastran.bdf.cards.methods.EIGPDefines poles that are used in complex eigenvalue extraction by the Determinant method
pyNastran.bdf.cards.methods.EIGRDefines data needed to perform real eigenvalue analysis
pyNastran.bdf.cards.methods.EIGRLDefines data needed to perform real eigenvalue (vibration or buckling) analysis with the Lanczos method
pyNastran.bdf.cards.baseCard.Element
pyNastran.f06.f06.EndOfFileError
pyNastran.op2.op2Errors.EndOfFileError
pyNastran.op2.tables.ept.EPT
pyNastran.gui.gui.EventsHandler
pyNastran.gui.box.Example
pyNastran.gui.gui.Example
pyNastran.f06.f06.F06
pyNastran.f06.f06Writer.F06Writer
pyNastran.bdf.cards.aero.FLFACTFLFACT SID F1 F2 F3 F4 F5 F6 F7 F8 F9 -etc
pyNastran.bdf.cards.aero.FLUTTERDefines data needed to perform flutter analysis
pyNastran.op2.tables.oug.oug_Objects.fluxObject
pyNastran.bdf.cards.loads.staticLoads.ForceGeneric class for all Forces
pyNastran.bdf.cards.loads.staticLoads.FORCE
pyNastran.bdf.cards.loads.staticLoads.FORCE1Defines a static concentrated force at a grid point by specification of a magnitude and two grid points that determine the direction
pyNastran.bdf.cards.loads.staticLoads.FORCE2Defines a static concentrated force at a grid point by specification of a magnitude and four grid points that determine the direction
pyNastran.op2.tables.opg_appliedLoads.opnl_forceVector.ForceVectorObject
pyNastran.op2.fortranFile.FortranFile
pyNastran.gui.demoGui.FrameVTK
pyNastran.bdf.cards.dynamic.FREQDefines a set of frequencies to be used in the solution of frequency response problems
pyNastran.bdf.cards.dynamic.FREQ1Defines a set of frequencies to be used in the solution of frequency response problems by specification of a starting frequency, frequency increment, and the number of increments desired
pyNastran.bdf.cards.dynamic.FREQ2Defines a set of frequencies to be used in the solution of frequency response problems by specification of a starting frequency, final frequency, and the number of logarithmic increments desired
pyNastran.bdf.cards.dynamic.FREQ4Defines a set of frequencies used in the solution of modal frequency response problems by specifying the amount of 'spread' around each natural frequency and the number of equally spaced excitation frequencies within the spread
pyNastran.op2.tables.geom.geom1.Geometry1
pyNastran.op2.tables.geom.geom2.Geometry2
pyNastran.op2.tables.geom.geom3.Geometry3
pyNastran.op2.tables.geom.geom4.Geometry4
pyNastran.op2.tables.geom.geometryTables.GeometryTables
pyNastran.op2.tables.geom.geometryTables.GeomObj
pyNastran.bdf.bdfInterface.getCard.GetMethods
pyNastran.bdf.cards.loads.staticLoads.GRAVDefines acceleration vectors for gravity or other acceleration loading GRAV SID CID A N1 N2 N3 MB GRAV 1 3 32.2 0.0 0.0 -1.0
pyNastran.bdf.cards.nodes.GRDSETDefines default options for fields 3, 7, 8, and 9 of all GRID entries
pyNastran.bdf.cards.nodes.GRID
pyNastran.bdf.cards.nodes.GRIDB
pyNastran.op2.tables.ogf_gridPointForces.ogf_Objects.gridPointForcesObject
pyNastran.op2.tables.ogf_gridPointForces.ogs_surfaceStresses.GridPointStressesObject
pyNastran.op2.tables.ogf_gridPointForces.ogs_surfaceStresses.GridPointStressesVolumeObject
pyNastran.bdf.cards.aero.GUSTDefines a stationary vertical gust for use in aeroelastic response analysis
pyNastran.op2.tables.oef_forces.oef_thermalObjects.HeatFlux_1D
pyNastran.op2.tables.oef_forces.oef_thermalObjects.HeatFlux_2D_3D
pyNastran.op2.tables.oef_forces.oef_thermalObjects.HeatFlux_CHBDYx
pyNastran.op2.tables.oef_forces.oef_thermalObjects.HeatFlux_CONV
pyNastran.op2.tables.oef_forces.oef_thermalObjects.HeatFlux_VU
pyNastran.op2.tables.oef_forces.oef_thermalObjects.HeatFlux_VU_3D
pyNastran.op2.tables.oef_forces.oef_thermalObjects.HeatFlux_VUBEAM
pyNastran.bdf.cards.materials.HyperelasticMaterialHyperelastic Material Class
pyNastran.op2.tables.oes_stressStrain.oes_nonlinear.HyperelasticQuadObject
pyNastran.general.logger.infoLogger
pyNastran.bdf.cards.properties.bars.IntegratedLineProperty
pyNastran::op2::op2Errors::InvalidCodeErrorGNU Lesser General Public License
pyNastran.op2.op2Errors.InvalidGridID_Error
pyNastran.op2.op2Errors.InvalidMarkerError
pyNastran.op2.op2Errors.InvalidMarkersError
pyNastran.bdf.cards.materials.IsotropicMaterialIsotropic Material Class
pyNastran.op2.tables.lama_eigenvalues.lama.LAMA
pyNastran.converters.LaWGS.wgsReader.LaWGS
pyNastran.converters.LaWGS.wgsIO.LaWGS_IO
pyNastran.converters.LaWGS.wgsReader.LaWGS_Panel
pyNastran.bdf.cards.elements.damper.LineDamper
pyNastran.bdf.cards.elements.bars.LineElement
pyNastran.bdf.cards.properties.bars.LineProperty
pyNastran.bdf.cards.loads.loads.LoadDefines the DefaultLoad class
pyNastran.bdf.cards.loads.staticLoads.LOAD
pyNastran.bdf.cards.loads.loads.LoadCombination
pyNastran.op2.tables.opg_appliedLoads.opg_loadVector.LoadVectorObject
pyNastran.bdf.cards.loads.loads.LSEQDefines a sequence of static load sets
pyNastran.bdf.cards.materials.MAT1Defines the material properties for linear isotropic materials
pyNastran.bdf.cards.materials.MAT10Defines material properties for fluid elements in coupled fluid-structural analysis
pyNastran.bdf.cards.materials.MAT2Defines the material properties for linear anisotropic materials for two-dimensional elements
pyNastran.bdf.cards.materials.MAT3Defines the material properties for linear orthotropic materials used by the CTRIAX6 element entry
pyNastran.bdf.cards.materials.MAT4Defines the constant or temperature-dependent thermal material properties for conductivity, heat capacity, density, dynamic viscosity, heat generation, reference enthalpy, and latent heat associated with a single-phase change
pyNastran.bdf.cards.materials.MAT5Defines the thermal material properties for anisotropic materials
pyNastran.bdf.cards.materials.MAT8Defines the material property for an orthotropic material for isoparametric shell elements
pyNastran.bdf.cards.materials.MAT9Defines the material properties for linear, temperature-independent, anisotropic materials for solid isoparametric elements (see PSOLID entry description)
pyNastran.bdf.cards.baseCard.MaterialBase Material Class
pyNastran.bdf.cards.materials.MaterialDependence
pyNastran.bdf.cards.materials.MATHP
pyNastran.f06.matlabWriter.MatlabWriter
pyNastran.bdf.cards.materials.MATS1Specifies stress-dependent material properties for use in applications involving nonlinear materials
pyNastran::f06::f06_classes::MaxDisplacementGNU Lesser General Public License
pyNastran.bdf.cards.methods.MethodGeneric class for all methods
pyNastran.bdf.cards.aero.MKAERO1Provides a table of Mach numbers (m) and reduced frequencies (k) for aerodynamic matrix calculation MKAERO1 m1 m2 m3 m4 m5 m6 m7 m8 k1 k2 k3 k4 k5 k6 k7 k8
pyNastran.bdf.cards.aero.MKAERO2Provides a table of Mach numbers (m) and reduced frequencies (k) for aerodynamic matrix calculation MKAERO2 m1 k1 m2 k2 m3 k3 m4 k4
pyNastran.bdf.cards.loads.staticLoads.MomentGeneric class for all Moments
pyNastran.bdf.cards.loads.staticLoads.MOMENT
pyNastran.bdf.cards.loads.staticLoads.MOMENT1
pyNastran.bdf.cards.loads.staticLoads.MOMENT2
pyNastran.gui.mouseStyle.MouseStyle
pyNastran.bdf.cards.constraints.MPC
pyNastran.bdf.cards.constraints.MPCADDDefines a multipoint constraint equation of the form \( \Sigma_j A_j u_j =0 \) where \( u_j \) represents degree-of-freedom \( C_j \) at grid or scalar point \( G_j \)
pyNastran.op2.tables.oqg_constraintForces.oqg_mpcForces.MPCForcesObject
pyNastran.op2.tables.mpt.MPT
pyNastran.gui.box.MyPopupMenu
pyNastran.gui.nastranIO.NastranIO
pyNastran.bdf.cards.dmig.NastranMatrixBase class for the DMIG, DMIJ, DMIJI, DMIK matrices
pyNastran.bdf.cards.dynamic.NLPARMDefines a set of parameters for nonlinear static analysis iteration strategy
pyNastran.bdf.cards.nodes.NodeGeneric Node base class
pyNastran.op2.tables.oef_forces.oef_Objects.nonlinearFluxObject
pyNastran.op2.tables.oes_stressStrain.oes_nonlinear.NonlinearQuadObject
pyNastran.op2.tables.oes_stressStrain.oes_nonlinear.NonlinearRodObject
pyNastran.bdf.cards.properties.mass.NSMDefines a set of non structural mass
pyNastran.op2.tables.oee_energy.oee.OEETable of energy
pyNastran.op2.tables.oef_forces.oef.OEFTable of element forces
pyNastran.op2.tables.oes_stressStrain.oes.OESTable of stresses/strains
pyNastran.f06.tables.oes.OES
pyNastran.op2.writer.oesWriter.Oes1Writer
pyNastran.op2.tables.oes_stressStrain.real.oes_objects.OES_Object
pyNastran.op2.tables.oes_stressStrain.oesnlxr.OESNLXRTable of stresses/strains
pyNastran.op2.tables.ogf_gridPointForces.ogf.OGFTable of Grid Point Forces
pyNastran.bdf.cards.loads.staticLoads.OneDeeLoad
pyNastran.op2.op2.OP2
pyNastran.op2.op2Codes.Op2Codes
pyNastran.op2.writer.op2Writer.Op2Writer
pyNastran.op2.tables.opg_appliedLoads.opg.OPGTable of element forces
pyNastran.bdf.cards.optimization.OptConstraint
pyNastran.f06.tables.oqg.OQG
pyNastran.op2.tables.oqg_constraintForces.oqg.OQGTable of spc/mpc forces/momenets
pyNastran.f06.tables.oug.OUG
pyNastran.op2.tables.oug.oug.OUGTable of displacements/velocities/acceleration/heat flux/temperature
pyNastran.op2.writer.ougWriter.Ougv1Writer
pyNastran.bdf.cards.aero.PAERO1Defines associated bodies for the panels in the Doublet-Lattice method
pyNastran.bdf.cards.aero.PAERO2Defines the cross-sectional properties of aerodynamic bodies PAERO2 PID ORIENT WIDTH AR LRSB LRIB LTH1 LTH2 THI1 THN1 THI2 THN2 THI3 THN3
pyNastran.gui.guiPanel.Pan
pyNastran.converters.panair.panairGrid.PanairGrid
pyNastran.converters.panair.panairGridPatch.PanairGridHelper
pyNastran.converters.panair.panairIO.PanairIO
pyNastran.converters.panair.panairGridPatch.PanairPatch
pyNastran.converters.panair.panairGridPatch.PanairWakePatch
pyNastran::converters::panair::panairWrite::PanairWriteGNU Lesser General Public License
pyNastran.bdf.cards.params.PARAM
pyNastran.bdf.errors.ParamParseError
pyNastran.bdf.cards.properties.bars.PBAR
pyNastran.bdf.cards.properties.bars.PBARL
pyNastran.bdf.cards.properties.bars.PBEAM
pyNastran.bdf.cards.properties.bars.PBEAM3
pyNastran.bdf.cards.properties.bars.PBEAML
pyNastran.bdf.cards.properties.bars.PBEND
pyNastran.bdf.cards.properties.bush.PBUSH
pyNastran.bdf.cards.properties.bush.PBUSH1D
pyNastran.bdf.cards.properties.shell.PCOMPPCOMP 701512 0.0+0 1.549-2 0.0+0 0.0+0 SYM 300704 3.7-2 0.0+0 YES 300704 3.7-2 45
pyNastran.bdf.cards.properties.shell.PCOMPG
pyNastran.bdf.cards.properties.properties.PCONEAX
pyNastran.bdf.cards.thermal.thermal.PCONVSpecifies the free convection boundary condition properties of a boundary condition surface element used for heat transfer analysis
pyNastran.bdf.cards.thermal.thermal.PCONVMSpecifies the free convection boundary condition properties of a boundary condition surface element used for heat transfer analysis
pyNastran.bdf.cards.properties.damper.PDAMP
pyNastran.bdf.cards.properties.damper.PDAMP5
pyNastran.bdf.cards.properties.damper.PDAMPT
pyNastran.bdf.cards.properties.springs.PELAS
pyNastran.bdf.cards.properties.springs.PELASTFrequency Dependent Elastic Property Defines the frequency dependent properties for a PELAS Bulk Data entry
pyNastran.bdf.cards.properties.properties.PFAST
pyNastran.bdf.cards.properties.properties.PGAP
pyNastran.bdf.cards.thermal.thermal.PHBDYA property entry referenced by CHBDYP entries to give auxiliary geometric information for boundary condition surface elements
pyNastran.op2.tables.oes_stressStrain.real.oes_plates.PlateStrainObject# ??? - is this just 11 ELEMENT STRAIN STRAINS IN ELEMENT COORD SYSTEM PRINCIPAL STRAINS (ZERO SHEAR) ID
pyNastran.op2.tables.oes_stressStrain.real.oes_plates.PlateStressObjectELEMENT FIBER STRESSES IN ELEMENT COORD SYSTEM PRINCIPAL STRESSES (ZERO SHEAR) ID
pyNastran.bdf.cards.loads.staticLoads.PLOAD
pyNastran.bdf.cards.loads.staticLoads.PLOAD1
pyNastran.bdf.cards.loads.staticLoads.PLOAD2
pyNastran.bdf.cards.loads.staticLoads.PLOAD4
pyNastran.bdf.cards.loads.staticLoads.PLOADX1
pyNastran.bdf.cards.properties.properties.PLSOLIDDefines a fully nonlinear (i.e., large strain and large rotation) hyperelastic solid element
pyNastran.bdf.cards.properties.mass.PMASS
pyNastran.bdf.cards.elements.mass.PointElement
pyNastran.bdf.cards.elements.mass.PointMass
pyNastran.bdf.cards.elements.mass.PointMassElement
pyNastran.bdf.cards.properties.mass.PointProperty
pyNastran.bdf.cards.properties.properties.PRAC2DCRAC2D Element Property Defines the properties and stress evaluation techniques to be used with the CRAC2D structural element
pyNastran.bdf.cards.properties.properties.PRAC3DCRAC3D Element Property Defines the properties of the CRAC3D structural element
pyNastran.bdf.cards.properties.bars.PROD
pyNastran.bdf.cards.baseCard.Property
pyNastran.bdf.cards.properties.shell.PSHEAR
pyNastran.bdf.cards.properties.shell.PSHELLPSHELL PID MID1 T MID2 12I/T**3 MID3 TS/T NSM Z1 Z2 MID4 PSHELL 41111 1 1.0000 1 1 0.02081
pyNastran.bdf.cards.properties.properties.PSOLIDPSOLID PID MID CORDM IN STRESS ISOP FCTN PSOLID 1 1 0 PSOLID 2 100 6 TWO GRID REDUCED
pyNastran.bdf.cards.properties.bars.PTUBE
pyNastran.bdf.cards.properties.damper.PVISC
pyNastran.gui.actionsControl.pyWidget
pyNastran.bdf.cards.thermal.loads.QBDY1Defines a uniform heat flux into CHBDYj elements
pyNastran.bdf.cards.thermal.loads.QBDY2Defines a uniform heat flux load for a boundary surface
pyNastran.bdf.cards.thermal.loads.QBDY3Defines a uniform heat flux load for a boundary surface
pyNastran.bdf.cards.thermal.loads.QHBDYDefines a uniform heat flux into a set of grid points
pyNastran.bdf.cards.sets.QSETDefines generalized degrees-of-freedom (q-set) to be used for dynamic reduction or component mode synthesis
pyNastran.bdf.cards.sets.QSET1Defines generalized degrees-of-freedom (q-set) to be used for dynamic reduction or component mode synthesis
pyNastran.bdf.cards.elements.shell.QuadShell
pyNastran.op2.tables.r1tab.R1TAB
pyNastran.bdf.cards.thermal.thermal.RADBCSpecifies an CHBDYi element face for application of radiation boundary conditions
pyNastran.bdf.cards.thermal.thermal.RADMDefines the radiation properties of a boundary element for heat transfer analysis
pyNastran.bdf.cards.sets.RADSETSpecifies which radiation cavities are to be included for radiation enclosure analysis
pyNastran.bdf.cards.loads.loads.RandomLoad
pyNastran.bdf.cards.tables.RandomTable
pyNastran.bdf.cards.loads.loads.RANDPSPower Spectral Density Specification Defines load set power spectral density factors for use in random analysis having the frequency dependent form:

\[ S_{jk}(F) = (X+iY)G(F) \]

pyNastran.bdf.cards.elements.rigid.RBAR
pyNastran.bdf.cards.elements.rigid.RBAR1
pyNastran.bdf.cards.elements.rigid.RBE1
pyNastran.bdf.cards.elements.rigid.RBE2
pyNastran.bdf.cards.elements.rigid.RBE3
pyNastran.op2.tables.oef_forces.oef_forceObjects.RealBendForce
pyNastran.op2.tables.oef_forces.oef_forceObjects.RealCBAR100Force
pyNastran.op2.tables.oef_forces.oef_forceObjects.RealCBARForce
pyNastran.op2.tables.oef_forces.oef_forceObjects.RealCBeamForce
pyNastran.op2.tables.oef_forces.oef_forceObjects.RealCBUSHForce
pyNastran.op2.tables.oef_forces.oef_forceObjects.RealCGAPForce
pyNastran.op2.tables.oef_forces.oef_forceObjects.RealConeAxForce
pyNastran.op2.tables.oef_forces.oef_forceObjects.RealCShearForce
pyNastran.op2.tables.oef_forces.oef_forceObjects.RealDamperForce
pyNastran.op2.tables.lama_eigenvalues.lama_objects.RealEigenvalues
pyNastran.op2.tables.oug.oug_eigenvectors.realEigenVectorObjectR E A L E I G E N V E C T O R N O
pyNastran.op2.tables.oes_stressStrain.real.elementsStressStrain.RealElementsStressStrain
pyNastran.op2.tables.oef_forces.oef_forceObjects.RealForce_VU
pyNastran.op2.tables.oef_forces.oef_forceObjects.RealForce_VU_2D
pyNastran.op2.tables.oef_forces.realForces.RealForces
pyNastran.op2.tables.oef_forces.oef_forceObjects.RealPentaPressureForce
pyNastran.op2.tables.oef_forces.oef_forceObjects.RealPLATE2Force
pyNastran.op2.tables.oef_forces.oef_forceObjects.RealPlateForce
pyNastran.op2.tables.oef_forces.oef_forceObjects.RealRodForce
pyNastran.op2.tables.oef_forces.oef_forceObjects.RealSpringForce
pyNastran.op2.tables.oef_forces.oef_forceObjects.RealViscForce
pyNastran.bdf.cards.coordinateSystems.RectangularCoord
pyNastran.op2.tables.resultTable.ResultTable
pyNastran.bdf.cards.loads.loads.RFORCE
pyNastran.bdf.cards.elements.rigid.RigidElement
pyNastran.bdf.cards.nodes.RingGeneric Ring base class
pyNastran.bdf.cards.nodes.RINGAXDefines a ring for conical shell problems RINGAX ID R Z PS RINGAX 3 2.0 -10.0 162
pyNastran.bdf.cards.loads.loads.RLOAD1Defines a frequency-dependent dynamic load of the form for use in frequency response problems
pyNastran.bdf.cards.loads.loads.RLOAD2Defines a frequency-dependent dynamic load of the form for use in frequency response problems
pyNastran.op2.tables.oes_stressStrain.real.oes_rods.RodDamperObject
pyNastran.bdf.cards.elements.bars.RodElement
pyNastran.op2.tables.oes_stressStrain.real.oes_rods.RodStrainObject# sCode=1 S T R A I N S I N R O D E L E M E N T S ( C R O D ) ELEMENT AXIAL SAFETY TORSIONAL SAFETY ID
pyNastran.op2.tables.oes_stressStrain.real.oes_rods.RodStressObject# formatCode=1 stressCode=0 S T R E S S E S I N R O D E L E M E N T S ( C R O D ) ELEMENT AXIAL SAFETY TORSIONAL SAFETY ELEMENT AXIAL SAFETY TORSIONAL SAFETY ID
pyNastran.op2.resultObjects.op2_Objects.scalarObject
pyNastran.bdf.errors.ScientificCardParseError
pyNastran.bdf.cards.sets.SEQSEPUsed with the CSUPER entry to define the correspondence of the exterior grid points between an identical or mirror-image superelement and its primary superelement
pyNastran.bdf.cards.sets.SESETDefines interior grid points for a superelement
pyNastran.bdf.cards.sets.SetGeneric Class all SETx cards inherit from
pyNastran.bdf.cards.sets.SET1Defines a list of structural grid points or element identification numbers
pyNastran.bdf.cards.sets.SET3Defines a list of grids, elements or points
pyNastran.bdf.cards.sets.SetSuperGeneric Class all Superelement SETx cards inherit from
pyNastran.op2.tables.oes_stressStrain.real.oes_shear.ShearStrainObject
pyNastran.op2.tables.oes_stressStrain.real.oes_shear.ShearStressObject# formatCode=1 sortCode=0 stressCode=0 S T R E S S E S I N S H E A R P A N E L S ( C S H E A R ) ELEMENT MAX AVG SAFETY ELEMENT MAX AVG SAFETY ID
pyNastran.bdf.cards.elements.shell.ShellElement
pyNastran.bdf.cards.properties.shell.ShellProperty
pyNastran.bdf.cards.loads.loads.SLOADStatic Scalar Load Defines concentrated static loads on scalar or grid points
pyNastran.bdf.cards.elements.solid.SolidElement
pyNastran.bdf.cards.properties.properties.SolidProperty
pyNastran.op2.tables.oes_stressStrain.real.oes_solids.SolidStrainObject# code=[1,0,11] S T R A I N S I N H E X A H E D R O N S O L I D E L E M E N T S ( H E X A ) CORNER ------CENTER AND CORNER POINT STRESSES--------- DIR
pyNastran.op2.tables.oes_stressStrain.real.oes_solids.SolidStressObject# sCode=0 N O N L I N E A R S T R E S S E S I N T E T R A H E D R O N S O L I D E L E M E N T S ( T E T R A ) ELEMENT GRID/ POINT STRESSES/ TOTAL STRAINS EQUIVALENT EFF
pyNastran.bdf.cards.constraints.SPCDefines enforced displacement/temperature (static analysis) velocity/acceleration (dynamic analysis) SPC SID G1 C1 D1 G2 C2 D2 SPC 2 32 3 -2.6 5
pyNastran.bdf.cards.constraints.SPC1SPC1 SID C G1 G2 G3 G4 G5 G6 G7 G8 G9 -etc
pyNastran.bdf.cards.constraints.SPCADDDefines a single-point constraint set as a union of single-point constraint sets defined on SPC or SPC1 entries
pyNastran.bdf.cards.constraints.SPCAXDefines a set of single-point constraints or enforced displacements for conical shell coordinates
pyNastran.bdf.cards.constraints.SPCDDefines an enforced displacement value for static analysis and an enforced motion value (displacement, velocity or acceleration) in dynamic analysis
pyNastran.op2.tables.oqg_constraintForces.oqg_spcForces.SPCForcesObject
pyNastran.bdf.cards.coordinateSystems.SphericalCoord

\[ r = \rho = \sqrt(x^2+y^2+z^2) \]

\[ \theta = tan^-1(\frac{y}{x}) \]

\[ \phi = cos^-1(\frac{z}{r}) \]

pyNastran.bdf.cards.aero.Spline
pyNastran.bdf.cards.aero.SPLINE1Surface Spline Methods Defines a surface spline for interpolating motion and/or forces for aeroelastic problems on aerodynamic geometries defined by regular arrays of aerodynamic points
pyNastran.bdf.cards.aero.SPLINE2Linear Spline Defines a surface spline for interpolating motion and/or forces for aeroelastic problems on aerodynamic geometries defined by regular arrays of aerodynamic points
pyNastran.bdf.cards.aero.SPLINE4Surface Spline Methods Defines a curved surface spline for interpolating motion and/or forces for aeroelastic problems on general aerodynamic geometries using either the Infinite Plate, Thin Plate or Finite Plate splining method
pyNastran.bdf.cards.aero.SPLINE5Linear Spline Defines a 1D beam spline for interpolating motion and/or forces for aeroelastic problems on aerodynamic geometries defined by irregular arrays of aerodynamic points
pyNastran.bdf.cards.nodes.SPOINT
pyNastran.bdf.cards.nodes.SPOINTsSPOINT ID1 ID2 ID3 ID4 ID5 ID6 ID7 ID8 or SPOINT ID1 THRU ID2 SPOINT 5 THRU 649
pyNastran.bdf.cards.elements.springs.SpringElement
pyNastran.bdf.cards.properties.springs.SpringProperty
pyNastran.op2.tables.oee_energy.oee_objects.StrainEnergyObjectE L E M E N T S T R A I N E N E R G I E S
pyNastran.op2.tables.oes_stressStrain.real.oes_objects.strainObject
pyNastran.op2.tables.oes_stressStrain.real.oes_objects.stressObject
pyNastran.bdf.subcase.Subcase
pyNastran.bdf.cards.constraints.SUPORTSUPORT ID1 C1 ID2 C2 ID3 C3 ID4 C4 SUPORT1 SID ID1 C1 ID2 C2 ID3 C3
pyNastran.bdf.cards.constraints.SUPORT1SUPORT1 SID ID1 C1 ID2 C2 ID3 C3
pyNastran.bdf.cards.tables.Table
pyNastran.bdf.cards.tables.TABLED1
pyNastran.bdf.cards.tables.TABLED2
pyNastran.bdf.cards.tables.TABLED3
pyNastran.bdf.cards.tables.TABLEM1
pyNastran.bdf.cards.tables.TABLEM2
pyNastran.bdf.cards.tables.TABLEM3
pyNastran.bdf.cards.tables.TABLEM4
pyNastran.bdf.cards.tables.TableObj
pyNastran.op2.resultObjects.tableObject.TableObject
pyNastran.bdf.cards.tables.TABLES1
pyNastran.bdf.cards.tables.TABLEST
pyNastran.bdf.cards.tables.TABRND1
pyNastran.bdf.cards.tables.TABRNDGGust Power Spectral Density Defines the power spectral density (PSD) of a gust for aeroelastic response analysis
pyNastran.bdf.cards.loads.loads.TabularLoad
pyNastran.op2.op2Errors.TapeCodeError
pyNastran.bdf.cards.thermal.loads.TEMPDefines temperature at grid points for determination of thermal loading, temperature-dependent material properties, or stress recovery
pyNastran.bdf.cards.thermal.loads.TEMPDDefines a temperature value for all grid points of the structural model that have not been given a temperature on a TEMP entry
pyNastran.op2.tables.oug.oug_temperatures.TemperatureObject
pyNastran.gui.gui.TestFrame
pyNastran.bdf.cards.thermal.thermal.ThermalBC
pyNastran.bdf.cards.thermal.thermal.ThermalCard
pyNastran.bdf.cards.thermal.thermal.ThermalElement
pyNastran.op2.tables.oef_forces.thermal_elements.ThermalElements
pyNastran.bdf.cards.thermal.loads.ThermalLoad
pyNastran.bdf.cards.thermal.loads.ThermalLoadDefault
pyNastran.op2.tables.opg_appliedLoads.opg_loadVector.ThermalLoadVectorObject
pyNastran.bdf.cards.materials.ThermalMaterialThermal Material Class
pyNastran.bdf.cards.thermal.thermal.ThermalProperty
pyNastran.op2.tables.opg_appliedLoads.opg_loadVector.ThermalVector
pyNastran.op2.tables.opg_appliedLoads.opg_loadVector.ThermalVelocityVectorObject
pyNastran.bdf.cards.tables.TICTransient Initial Condition
pyNastran.bdf.cards.loads.loads.TLOAD1Transient Response Dynamic Excitation, Form 1 Defines a time-dependent dynamic load or enforced motion of the form:

\[ {P(t)} = {A} \cdot F(t-\tau) \]

for use in transient response analysis

pyNastran.bdf.cards.loads.loads.TLOAD2Transient Response Dynamic Excitation, Form 1 Defines a time-dependent dynamic load or enforced motion of the form:

\[ {P(t)} = {A} \cdot F(t-\tau) \]

for use in transient response analysis

pyNastran.op2.tables.oes_stressStrain.real.oes_triax.TriaxStrainObject# formatCode=1 sortCode=0 stressCode=0 S T R A I N S I N T R I A X 6 E L E M E N T S ELEMENT GRID ID STRAINS IN MATERIAL COORD SYSTEM MAX MAG MAX VON MISES ID RADIAL AZIMUTHAL AXIAL SHEAR PRINCIPAL SHEAR 5351 0 -9.726205E+02 -1.678908E+03 -1.452340E+03 -1.325111E+02 -1.678908E+03 3.702285E+02 6.654553E+02 4389 -9.867789E+02 -1.624276E+03 -1.388424E+03 -9.212539E+01 -1.624276E+03 3.288099E+02 5.806334E+02
pyNastran.op2.tables.oes_stressStrain.real.oes_triax.TriaxStressObject# formatCode=1 sortCode=0 stressCode=0 S T R E S S E S I N T R I A X 6 E L E M E N T S ELEMENT GRID ID STRESSES IN MATERIAL COORD SYSTEM MAX MAG MAX VON MISES ID RADIAL AZIMUTHAL AXIAL SHEAR PRINCIPAL SHEAR 5351 0 -9.726205E+02 -1.678908E+03 -1.452340E+03 -1.325111E+02 -1.678908E+03 3.702285E+02 6.654553E+02 4389 -9.867789E+02 -1.624276E+03 -1.388424E+03 -9.212539E+01 -1.624276E+03 3.288099E+02 5.806334E+02
pyNastran.bdf.cards.aero.TRIM
pyNastran.bdf.cards.elements.shell.TriShell
pyNastran.bdf.cards.dynamic.TSTEPTransient Time Step Defines time step intervals at which a solution will be generated and output in transient analysis
pyNastran.bdf.cards.dynamic.TSTEPNLDefines parametric controls and data for nonlinear transient structural or heat transfer analysis
pyNastran.op2.tables.oug.oug_velocities.VelocityObject
pyNastran.bdf.bdfInterface.bdf_writeMesh.WriteMesh
pyNastran.bdf.bdfInterface.crossReference.XrefMeshLinks up the various cards in the BDF
pyNastran.op2.op2Errors.ZeroBufferError
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