pyNastran.bdf.cards.sets.ABCQSet | Generic Class ASET, BSET, CSET, QSET cards inherit from |
pyNastran.bdf.cards.sets.ABQSet1 | Generic Class ASET1, BSET1, QSET1 cards inherit from |
pyNastran.bdf.cards.loads.staticLoads.ACCEL1 | Acceleration 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.AEFACT | Defines real numbers for aeroelastic analysis |
pyNastran.bdf.cards.aero.AELINK | Defines 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.AELIST | Defines a list of aerodynamic elements to undergo the motion prescribed with the AESURF Bulk Data entry for static aeroelasticity |
pyNastran.bdf.cards.aero.AEPARM | Defines a general aerodynamic trim variable degree-of-freedom (aerodynamic extra point) |
pyNastran.bdf.cards.aero.Aero | Base class for AERO and AEROS cards |
pyNastran.bdf.cards.aero.AERO | Gives basic aerodynamic parameters for unsteady aerodynamics |
pyNastran.bdf.cards.aero.AEROS | Gives basic aerodynamic parameters for unsteady aerodynamics |
pyNastran.bdf.cards.aero.AESTAT | Specifies rigid body motions to be used as trim variables in static aeroelasticity |
pyNastran.bdf.cards.aero.AESURF | Specifies an aerodynamic control surface as a member of the set of aerodynamic extra points |
pyNastran.bdf.cards.aero.AESURFS | Optional 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.AnisotropicMaterial | Anisotropic Material Class |
pyNastran.gui.gui.AppFrame | |
pyNastran.op2.tables.opg_appliedLoads.opg_Objects.AppliedLoadsObject | |
pyNastran.bdf.cards.sets.ASET | Defines degrees-of-freedom in the analysis set (a-set) |
pyNastran.bdf.cards.sets.ASET1 | Defines 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.BDF | NASTRAN 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.BSET | Defines 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.CAERO1 | Defines an aerodynamic macro element (panel) in terms of two leading edge locations and side chords |
pyNastran.bdf.cards.aero.CAERO2 | Aerodynamic 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::CardParseError | GNU 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.CBAR | CBAR 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.CBEAM | CBEAM 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.CBEAM3 | Defines 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.CBUSH2D | 2-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.CelasStressObject | S 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.CHBDYE | Defines a boundary condition surface element with reference to a heat conduction element |
pyNastran.bdf.cards.thermal.thermal.CHBDYG | Defines a boundary condition surface element without reference to a property entry |
pyNastran.bdf.cards.thermal.thermal.CHBDYP | Defines a boundary condition surface element with reference to a PHBDY entry |
pyNastran.bdf.cards.elements.solid.CHEXA20 | CHEXA 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.CHEXA8 | CHEXA EID PID G1 G2 G3 G4 G5 G6 G7 G8 |
pyNastran.bdf.cards.elements.mass.CMASS1 | Defines a scalar mass element |
pyNastran.bdf.cards.elements.mass.CMASS2 | Defines a scalar mass element without reference to a property entry |
pyNastran.bdf.cards.elements.mass.CMASS3 | Defines a scalar mass element that is connected only to scalar points |
pyNastran.bdf.cards.elements.mass.CMASS4 | Defines 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.ComplexCelasStressObject | S 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.ComplexPlateStressObject | C 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.CONV | Specifies 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.CORD3G | Defines a general coordinate system using three rotational angles as functions of coordinate values in the reference coordinate system |
pyNastran.bdf.cards.elements.solid.CPENTA15 | CPENTA EID PID G1 G2 G3 G4 G5 G6 G7 G8 G9 G10 G11 G12 G13 G14 G15 |
pyNastran.bdf.cards.elements.solid.CPENTA6 | CPENTA 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.CSET | Defines 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.CSET1 | Defines 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.CSSCHD | Defines a scheduled control surface deflection as a function of Mach number and angle of attack |
pyNastran.bdf.cards.elements.solid.CTETRA10 | CTETRA 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.CTETRA4 | CTETRA 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.CTRIAX6 | Nodes 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.DAREA | Defines 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.DMIG | Defines direct input matrices related to grid, extra, and/or scalar points |
pyNastran.bdf.cards.dmig.DMIJ | Direct 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.DMIJI | Direct 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.DMIK | Direct 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.EIGB | Defines data needed to perform buckling analysis |
pyNastran.bdf.cards.methods.EIGC | Defines data needed to perform complex eigenvalue analysis |
pyNastran.op2.tables.oug.oug_eigenvectors.EigenVectorObject | EIGENVALUE = 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.EIGP | Defines poles that are used in complex eigenvalue extraction by the Determinant method |
pyNastran.bdf.cards.methods.EIGR | Defines data needed to perform real eigenvalue analysis |
pyNastran.bdf.cards.methods.EIGRL | Defines 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.FLFACT | FLFACT SID F1 F2 F3 F4 F5 F6 F7 F8 F9 -etc |
pyNastran.bdf.cards.aero.FLUTTER | Defines data needed to perform flutter analysis |
pyNastran.op2.tables.oug.oug_Objects.fluxObject | |
pyNastran.bdf.cards.loads.staticLoads.Force | Generic class for all Forces |
pyNastran.bdf.cards.loads.staticLoads.FORCE | |
pyNastran.bdf.cards.loads.staticLoads.FORCE1 | Defines 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.FORCE2 | Defines 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.FREQ | Defines a set of frequencies to be used in the solution of frequency response problems |
pyNastran.bdf.cards.dynamic.FREQ1 | Defines 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.FREQ2 | Defines 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.FREQ4 | Defines 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.GRAV | Defines 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.GRDSET | Defines 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.GUST | Defines 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.HyperelasticMaterial | Hyperelastic Material Class |
pyNastran.op2.tables.oes_stressStrain.oes_nonlinear.HyperelasticQuadObject | |
pyNastran.general.logger.infoLogger | |
pyNastran.bdf.cards.properties.bars.IntegratedLineProperty | |
pyNastran::op2::op2Errors::InvalidCodeError | GNU Lesser General Public License |
pyNastran.op2.op2Errors.InvalidGridID_Error | |
pyNastran.op2.op2Errors.InvalidMarkerError | |
pyNastran.op2.op2Errors.InvalidMarkersError | |
pyNastran.bdf.cards.materials.IsotropicMaterial | Isotropic 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.Load | Defines 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.LSEQ | Defines a sequence of static load sets |
pyNastran.bdf.cards.materials.MAT1 | Defines the material properties for linear isotropic materials |
pyNastran.bdf.cards.materials.MAT10 | Defines material properties for fluid elements in coupled fluid-structural analysis |
pyNastran.bdf.cards.materials.MAT2 | Defines the material properties for linear anisotropic materials for two-dimensional elements |
pyNastran.bdf.cards.materials.MAT3 | Defines the material properties for linear orthotropic materials used by the CTRIAX6 element entry |
pyNastran.bdf.cards.materials.MAT4 | Defines 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.MAT5 | Defines the thermal material properties for anisotropic materials |
pyNastran.bdf.cards.materials.MAT8 | Defines the material property for an orthotropic material for isoparametric shell elements |
pyNastran.bdf.cards.materials.MAT9 | Defines the material properties for linear, temperature-independent, anisotropic materials for solid isoparametric elements (see PSOLID entry description) |
pyNastran.bdf.cards.baseCard.Material | Base Material Class |
pyNastran.bdf.cards.materials.MaterialDependence | |
pyNastran.bdf.cards.materials.MATHP | |
pyNastran.f06.matlabWriter.MatlabWriter | |
pyNastran.bdf.cards.materials.MATS1 | Specifies stress-dependent material properties for use in applications involving nonlinear materials |
pyNastran::f06::f06_classes::MaxDisplacement | GNU Lesser General Public License |
pyNastran.bdf.cards.methods.Method | Generic class for all methods |
pyNastran.bdf.cards.aero.MKAERO1 | Provides 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.MKAERO2 | Provides 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.Moment | Generic 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.MPCADD | Defines 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.NastranMatrix | Base class for the DMIG, DMIJ, DMIJI, DMIK matrices |
pyNastran.bdf.cards.dynamic.NLPARM | Defines a set of parameters for nonlinear static analysis iteration strategy |
pyNastran.bdf.cards.nodes.Node | Generic 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.NSM | Defines a set of non structural mass |
pyNastran.op2.tables.oee_energy.oee.OEE | Table of energy |
pyNastran.op2.tables.oef_forces.oef.OEF | Table of element forces |
pyNastran.op2.tables.oes_stressStrain.oes.OES | Table 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.OESNLXR | Table of stresses/strains |
pyNastran.op2.tables.ogf_gridPointForces.ogf.OGF | Table 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.OPG | Table of element forces |
pyNastran.bdf.cards.optimization.OptConstraint | |
pyNastran.f06.tables.oqg.OQG | |
pyNastran.op2.tables.oqg_constraintForces.oqg.OQG | Table of spc/mpc forces/momenets |
pyNastran.f06.tables.oug.OUG | |
pyNastran.op2.tables.oug.oug.OUG | Table of displacements/velocities/acceleration/heat flux/temperature |
pyNastran.op2.writer.ougWriter.Ougv1Writer | |
pyNastran.bdf.cards.aero.PAERO1 | Defines associated bodies for the panels in the Doublet-Lattice method |
pyNastran.bdf.cards.aero.PAERO2 | Defines 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::PanairWrite | GNU 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.PCOMP | PCOMP 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.PCONV | Specifies the free convection boundary condition properties of a boundary condition surface element used for heat transfer analysis |
pyNastran.bdf.cards.thermal.thermal.PCONVM | Specifies 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.PELAST | Frequency 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.PHBDY | A 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.PlateStressObject | ELEMENT 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.PLSOLID | Defines 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.PRAC2D | CRAC2D Element Property Defines the properties and stress evaluation techniques to be used with the CRAC2D structural element |
pyNastran.bdf.cards.properties.properties.PRAC3D | CRAC3D 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.PSHELL | PSHELL 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.PSOLID | PSOLID 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.QBDY1 | Defines a uniform heat flux into CHBDYj elements |
pyNastran.bdf.cards.thermal.loads.QBDY2 | Defines a uniform heat flux load for a boundary surface |
pyNastran.bdf.cards.thermal.loads.QBDY3 | Defines a uniform heat flux load for a boundary surface |
pyNastran.bdf.cards.thermal.loads.QHBDY | Defines a uniform heat flux into a set of grid points |
pyNastran.bdf.cards.sets.QSET | Defines generalized degrees-of-freedom (q-set) to be used for dynamic reduction or component mode synthesis |
pyNastran.bdf.cards.sets.QSET1 | Defines 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.RADBC | Specifies an CHBDYi element face for application of radiation boundary conditions |
pyNastran.bdf.cards.thermal.thermal.RADM | Defines the radiation properties of a boundary element for heat transfer analysis |
pyNastran.bdf.cards.sets.RADSET | Specifies 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.RANDPS | Power 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.realEigenVectorObject | R 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.Ring | Generic Ring base class |
pyNastran.bdf.cards.nodes.RINGAX | Defines a ring for conical shell problems RINGAX ID R Z PS RINGAX 3 2.0 -10.0 162 |
pyNastran.bdf.cards.loads.loads.RLOAD1 | Defines a frequency-dependent dynamic load of the form for use in frequency response problems |
pyNastran.bdf.cards.loads.loads.RLOAD2 | Defines 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.SEQSEP | Used 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.SESET | Defines interior grid points for a superelement |
pyNastran.bdf.cards.sets.Set | Generic Class all SETx cards inherit from |
pyNastran.bdf.cards.sets.SET1 | Defines a list of structural grid points or element identification numbers |
pyNastran.bdf.cards.sets.SET3 | Defines a list of grids, elements or points |
pyNastran.bdf.cards.sets.SetSuper | Generic 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.SLOAD | Static 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.SPC | Defines 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.SPC1 | SPC1 SID C G1 G2 G3 G4 G5 G6 G7 G8 G9 -etc |
pyNastran.bdf.cards.constraints.SPCADD | Defines a single-point constraint set as a union of single-point constraint sets defined on SPC or SPC1 entries |
pyNastran.bdf.cards.constraints.SPCAX | Defines a set of single-point constraints or enforced displacements for conical shell coordinates |
pyNastran.bdf.cards.constraints.SPCD | Defines 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.SPLINE1 | Surface 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.SPLINE2 | Linear 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.SPLINE4 | Surface 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.SPLINE5 | Linear 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.SPOINTs | SPOINT 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.StrainEnergyObject | E 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.SUPORT | SUPORT ID1 C1 ID2 C2 ID3 C3 ID4 C4 SUPORT1 SID ID1 C1 ID2 C2 ID3 C3 |
pyNastran.bdf.cards.constraints.SUPORT1 | SUPORT1 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.TABRNDG | Gust 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.TEMP | Defines temperature at grid points for determination of thermal loading, temperature-dependent material properties, or stress recovery |
pyNastran.bdf.cards.thermal.loads.TEMPD | Defines 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.ThermalMaterial | Thermal 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.TIC | Transient Initial Condition |
pyNastran.bdf.cards.loads.loads.TLOAD1 | Transient 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.TLOAD2 | Transient 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.TSTEP | Transient Time Step Defines time step intervals at which a solution will be generated and output in transient analysis |
pyNastran.bdf.cards.dynamic.TSTEPNL | Defines 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.XrefMesh | Links up the various cards in the BDF |
pyNastran.op2.op2Errors.ZeroBufferError | |