Description | |
CBAR | Defines a simple beam element. (p. 60) |
CBEAM | Defines a beam element. (p. 62) |
CBEND | |
CDAMP1 | Defines a scalar damper element. (p. 60) |
CELAS1 | Defines a scalar spring element. (p. 60) |
CHBDYG | Defines a boundary condition surface element without reference to a property entry. (p. 71) |
CHBDYP | |
CHEXA | Defines the connections of the six-sided solid element with eight to twenty grid points. (p. 65) |
CONROD | Defines a rod element without reference to a property entry.(p. 110) |
CONV | |
CONVM | |
CORD2C | Defines a cylindrical coordinate system using the coordinates of three points. (p. 51) |
CORD2R | Defines a rectangular coordinate system using the coordinates of three points. (p. 51) |
CORD2S | Defines a spherical coordinate system using the coordinates of three points. (p. 51) |
CPENTA | Defines the connections of a five-sided solid element with six to fifteen grid points. (p. 65) |
CQUAD4 | |
CQUAD8 | Defines a curved quadrilateral shell or plane strain element with eight grid points. (p. 64) |
CROD | Defines a tension-compression-torsion element. (p. 60) |
CTETRA | Defines the connections of the four-sided solid element with four to ten grid points. (p. 65) |
CTRIA3 | Defines an isoparametric membrane-bending or plane strain triangular plate element. (p. 64) |
CTRIA6 | Defines a curved triangular shell element or plane strain with six grid points. (p. 64) |
CTRIAX6 | Defines an isoparametric and axisymmetric triangular cross section ring element with midside grid points. (p. 65) |
CTUBE | Defines a tension-compression-torsion tube element. (p. 63) |
DLOAD | Defines a dynamic loading condition for frequency response or transient response problems as a linear combination of load sets defined via RLOAD1 or RLOAD2 entries for frequency response or TLOAD1 or TLOAD2 entries for transient response. (p. 66) |
INCLUDE | Inserts an external file into the input file. The INCLUDE statement may appear anywhere within the input data file. (p. 109) |
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. (p. 53) |
MAT5 | Defines the thermal material properties for anisotropic materials. (p. 53) |
MATT4 | Specifies table references for temperature-dependent MAT4 material properties. (p. 53) |
MATT5 | Specifies temperature-dependent material properties on MAT5 entry fields via TABLEMi entries. (p. 53) |
MPC | Defines a multipoint constraint equation of the form. (p. 50) |
NLPARM | |
PARAM,AUTOSPC | AUTOSPC specifies the action to take when singularities exist in the stiffness matrix [Kgg]. AUTOSPC = YES means that singularities will be constrained automatically. AUTOSPC = NO means that singularities will not be constrained. (p. 114) |
PARAM,PRGPST | Controls the printout of singularities. See AUTOSPC. Default = YES. (p. 117) |
PARAM,SIGMA | The radiant heat flux is proportional to SIGMA*(Tgrid + TABS)4, where SIGMA is the Stefan-Boltzmann constant. Default = 0.0. (p. 115) |
PARAM,TABS | TABS is used to convert units of the temperature input (oF or oC) to the absolute temperature (°R or °K). Default = 0.0. (p. 115) |
PBAR | Defines the properties of a simple beam element (CBAR entry). (p. 60) |
PBEAM | Defines the properties of a beam element (CBEAM entry). This element may be used to model tapered beams. (p. 62) |
PBEND | |
PCONV | |
PCONVM | |
PDAMP | Specifies the damping value of a scalar damper element using defined CDAMP1 or CDAMP3 entries. (p. 60) |
PELAS | Specifies the stiffness, damping coefficient, and stress coefficient of a scalar elastic (spring) element (CELAS1 or CELAS3 entry). (p. 60) |
PHBDY | |
PROD | Defines the properties of a rod element (CROD entry). (p. 60) |
PSHELL | Defines the membrane, bending, transverse shear, and coupling properties of thin shell elements. (p. 64) |
PSOLID | Defines the properties of solid elements (CHEXA, CPENTA, and CTETRA entries). (p. 65) |
PTUBE | Defines the properties of a thin-walled cylindrical tube element (CTUBE entry). (p. 63) |
QBDY2 | Defines grid point heat flux into CHBDYi elements. (p. 76) |
QBDY3 | Defines a uniform heat flux load for a boundary surface. (p. 76) |
QHBDY | Defines a uniform heat flux load into a set of grid points. (p. 79) |
QVECT | Defines thermal vector flux from a distant source into a face of one or more CHBDYi boundary condition surface elements. (p. 77) |
QVOL | |
RADBC | |
RADCAV | |
RADM | |
RADMT | |
RADSET | Specifies which radiation cavities are to be included for radiation enclosure analysis. (p. 98) |
SLOAD | Defines concentrated static loads on scalar or grid points. (p. 79) |
SPC | Defines a set of single point constraints and enforced displacements. (p. 73) |
SPOINT | |
TABLED1 | Defines a tabular function for use in generating frequency-dependent and time-dependent dynamic loads. (p. 71) |
TABLEM1 | |
TEMP | Defines temperature at grid points for determination of thermal loading, temperature-dependent material properties, or stress recovery. (p. 75) |
TEMPBC | Defines the temperature boundary conditions for heat transfer analysis. Applies to steady state and transient conditions. (p. 73) |
TEMPD | |
TLOAD1 | |
TSTEPNL | |
VIEW | Defines radiation cavity and shadowing for radiation view factor calculations. (p. 98) |
VIEW3D | Defines parameters to control and/or request the Gaussian Integration method of view factor calculation for a specified cavity. (p. 115) |