Altair OptiStruct Online Help
- 1
- 1D beam modeling - aerospace[1]
- 1D elements[1]
- 1-plane symmetry constraint[1]
- 3
- 3D (rounded edges) contacts benchmark 2[1]
- 3D loaded pin test problem[1]
- 3D sheet metal forming problem[1]
- 3D steel roller on rubber problem[1]
- 3-point bending simulation - hi-tech electronic applications[1]
- 3-point bending using RBODY example[1]
- _
- _bdst.mvw file[1]
- _des.h3d file[1]
- _e.nlm file[1]
- _err.grid file[1]
- _fat.#.eqsts file[1]
- _frames.html file[1]
- _freq.#.mvw file[1]
- _freq.mvw file[1]
- _gauge.h3d file[1]
- _gso.slk file[1]
- _hist.mvw file[1]
- _ld.monitor file[1]
- _mass.#.mvw file[1]
- _mass.mvw file[1]
- _mbd.h3d file[1]
- _mbd.log file[1]
- _mbd.mrf file[1]
- _mbd.mvw file[1]
- _mbd.xml file[1]
- _menu.html file[1]
- _modal.#.mvw file[1]
- _modal.mvw file[1]
- _nlm.mvw file[1]
- _rand.mvw file[1]
- _s#_a.#.frf file[1]
- _s#_a.frf file[1]
- _s#_a.mbd file[1]
- _s#_a.trn file[1]
- _s#_d.#.frf file[1]
- _s#_d.frf file[1]
- _s#_d.mbd file[1]
- _s#_d.trn file[1]
- _s#_v.#.frf file[1]
- _s#_v.frf file[1]
- _s#_v.mbd file[1]
- _s#_v.trn file[1]
- _s#.h3d file[1]
- _sens.#.mvw file[1]
- _shuffling.#.fem file[1]
- _sizing.#.fem file[1]
- _sizing.#.inc file[1]
- _topol.h3d file[1]
- _tran.mvw file[1]
- .
- .#.#.#.dis file[1]
- .#.#.dis.# file[1]
- .#.#.dis file[1]
- .#.#.els file[1]
- .#.#.fat file[1]
- .#.dis.# file[1]
- .#.dis file[1]
- .#.eigv file[1]
- .#.els.# file[1]
- .#.els file[1]
- .#.grid file[1]
- .#.h3d file[1]
- .#.mass file[1]
- .#.rnf file[1]
- .#.sens file[1]
- .#.sh file[1]
- .#.slk file[1]
- .amls_singularity.cmf file[1]
- .amses_singularity.cmf file[1]
- .bdst file[1]
- .cntf file[1]
- .contgap.fem file[1]
- .cpr file[1]
- .cstr file[1]
- .dens file[1]
- .desvar file[1]
- .dis.# file[1]
- .disp file[1]
- .dvgrid file[1]
- .echo file[1]
- .els.# file[1]
- .force file[1]
- .fsthick file[1]
- .full.mat file[1]
- .gpf file[1]
- .grid file[1]
- .h3d file[1]
- .hdf5 file[1]
- .hgdata file[1]
- .hist file[1]
- .HM.autospc.cmf file[1]
- .HM.comp.tcl file[1]
- .HM.conn.tcl file[1]
- .HM.crtelem.cmf file[1]
- .HM.elcheck.###.cmf file[1]
- .HM.elcheck.cmf file[1]
- .HM.ent.tcl file[1]
- .HM.gapstat.cmf file[1]
- .html file[1]
- .interface file[1]
- .joint file[1]
- .k.op2 file[1]
- .kpi file[1]
- .load file[1]
- .m.op2 file[1]
- .mass file[1]
- .mgg file[1]
- .mnf file[1]
- .monitor file[1]
- .mpcf file[1]
- .op2 file[1]
- .oss file[1]
- .out file[1]
- .pch file[1]
- .pcomp file[1]
- .peak file[1]
- .pret file[1]
- .prop file[1]
- .rand file[1]
- .reduced.mat file[1]
- .rengy file[1]
- .res file[1]
- .secres file[1]
- .seplot file[1]
- .sh file[1]
- .spcd file[1]
- .spcf file[1]
- .stat file[1]
- .strn file[1]
- .strs file[1]
- @
- @hyperform -I/O options and subcase information entry[1]
- <
- A
- A2GG - subcase information entry[1]
- ACCEL1 -[1]
- ACCEL2 -[1]
- ACCEL -[1]
- ACCELERATION - I/O options and subcase information entry[1]
- acceleration punch file[1]
- acceleration punch file - frequency response analysis[1]
- acceleration punch file - linear transient analysis[1]
- acceleration punch file - linear transient analysis by Fourier transformation[1]
- acceleration punch file - random response analysis[1]
- accessing model files[1]
- access model files[1]
- access model files - verification problem[1][2]
- ACCLR -[1]
- ACDISP -[1]
- ACINT - I/O Options Entry[1]
- ACMODL -[1]
- acoustic analysis[1]
- acoustic analysis - coupled FRF analysis[1]
- acoustic analysis of a 2.1 speaker using infinite elements[1]
- acoustic infinite elements[1]
- acoustic infinite elements - implementation[1]
- acoustic infinite elements - input/output[1]
- acoustic performance analysis - hi-tech electronic applications[1]
- ACPOWER - I/O Options Entry[1]
- ACPVELO - I/O Options Entry[1]
- ACSRCE -[1]
- ADAMS[1]
- adhesive/bonded interface implementation methods - cohesive zone modeling[1]
- advanced small displacement fea tutorials[1]
- aerospace applications[1]
- aerospace - design optimization[1]
- aerospace - FEM[1]
- aerospace - solution sequences[1]
- aerospace - summary[1]
- air conditioner bracket example - topology optimization[1]
- aircraft fitting analysis - aerospace[1]
- airframe stress anlaysis - aerospace[1]
- AMLS - solvers[1]
- AMSES - solvers[1]
- analysis of composite shells[1]
- analysis of pressure vessel (plane strain)[1]
- analysis of pretensioned assemblies[1]
- analysis output - defaults[1]
- ANALYSIS - subcase information entry[1]
- analysis techniques[1]
- analytical background - radiated sound output[1]
- and guidelines[1]
- appendix - internal responses[1]
- appendix - parts and instances[1]
- applied forces and motions - MBD[1]
- apply heat flux loads[1][2]
- arbitrary beam section definition[1]
- ASET1 -[1]
- ASET -[1]
- ASSEMBLY -[1]
- ASSIGN -[1]
- automated reanalysis - lattice structure optimization[1]
- automated transfer path analysis process - nvh[1]
- automatic multi-level sub-structuring[1]
- Automatic Multi-level Sub-structuring Eigensolver[1]
- automatic time stepping - nonlinear direct transient analysis[1]
- AUTOSPC -[1]
- AVL EXCITE[1]
- axisymmetric element property[1]
- B
- B2GG - subcase information entry[1]
- ball impact on cell phone analysis - hi-tech electronic applications[1]
- basic checks - debugging guide[1]
- basic small displacement fea tutorials[1]
- battery pack bending simulation - hi-tech electronic applications[1]
- BCS - solvers[1]
- BEAD -[1]
- beam bending using nonlinear transient analysis example[1]
- BEGIN -[1]
- BLKHDF -[1]
- BMFACE -[1]
- BNDFIX1 -[1]
- BNDFIX -[1]
- BNDFRE1 -[1]
- BNDFREE -[1]
- bodies - MBD[1]
- BORE -[1]
- bore distortion responses[1]
- boundary conditions for structural analysis and optimization[1]
- brake squeal analysis[1]
- brake squeal analysis - implementation[1]
- brake squeal analysis - input/output[1]
- BSET1 -[1]
- BSET -[1]
- buckling analysis - linear[1]
- buckling of shells and composites with offset[1]
- buckling problems - debug methods[1]
- build external libraries[1]
- build external libraries - optimization responses[1]
- bulk data entries by function[1]
- bulk data entries by function for explicit analysis[1]
- bulk data input file[1]
- bulk data section[1]
- C
- CAABSF -[1]
- CACINF3 -[1]
- CACINF4 -[1]
- campbell diagram - rotor dynamics[1]
- cantilever beam in bending example[1]
- cantilevered tapered membrane (Test No. FV32)[1]
- cantilevered thin square plate (test no. FV16)[1]
- cantilever with off-center point masses (Test No. FV4)[1]
- capabilities[1]
- car bumper impact using nonlinear transient analysis[1]
- CBAR -[1]
- CBEAM -[1]
- CBUSH1D -[1]
- CBUSH -[1]
- CDAMP1 -[1]
- CDAMP2 -[1]
- CDAMP3 -[1]
- CDAMP4 -[1]
- CDSMETH -[1][2]
- cds superelement[1]
- CELAS1 -[1]
- CELAS2 -[1]
- CELAS2F -[1]
- CELAS3 -[1]
- CELAS4 -[1]
- CELAS4F -[1]
- CELL -[1]
- cell phone drop test - hi-tech electronic applications[1]
- CFAILURE -[1]
- CFAST -[1]
- CGAP -[1]
- CGAPG -[1]
- CGASK6 -[1]
- CGASK6 element checks and default bound values[1]
- CGASK8 -[1]
- CGASK8 element checks and default bound values[1]
- CGASK12 -[1]
- CGASK12 element checks and default bound values[1]
- CGASK16 -[1]
- CGASK16 element checks and default bound values[1]
- CHACAB -[1]
- change length of bodies - MBD system level response optimization[1]
- CHBDYE -[1]
- CHECK -[1]
- CHEXA -[1]
- CHEXA element checks and default bound values[1]
- CIFHEX -[1]
- CIFPEN -[1]
- clamped thick rhombic plate (Test No. FV22)[1]
- clamped thin rhombic plate (Test No. FV15)[1]
- CMASS1 -[1]
- CMASS2 -[1]
- CMASS3 -[1]
- CMASS4 -[1]
- CMBEAM -[1]
- CMBEAMM -[1]
- CMBUSH -[1]
- CMBUSHC -[1]
- CMBUSHE -[1]
- CMBUSHM -[1]
- CMBUSHT -[1]
- CMDE -[1]
- CMETHOD - subcase information entry[1]
- CMKE -[1]
- CMSE -[1]
- CMSMETH -[1]
- CMSMETH - subcase information entry[1]
- CMSPDP -[1]
- CMSPDPC -[1]
- CMSPDPE -[1]
- CMSPDPM -[1]
- CMSPDPT -[1]
- CNTNLSUB - subcase information entry[1]
- CNTSTB -[1]
- CNTSTB - subcase information entry[1]
- cohesive zone modeling[1]
- combination joints (elements)[1]
- Combined Topology and Topography Tutorials[1]
- combine pattern repetition and pattern grouping with other manufacturing constraints[1]
- complex eigenvalue analysis[1]
- compliance management - lattice structure optimization[1]
- compliant elements - MBD[1]
- component dynamic analysis (cdsmeth) superelement generation[1]
- composite laminates[1]
- composite problems - debug methods[1]
- composite shell bending[1]
- composite structures[1]
- composite structures - free-sizing[1]
- composite structures - phase transitions[1]
- composite structures - ply-based sizing[1]
- composite structures - stacking sequence[1]
- composite topology and free-size optimization[1]
- composite topology and free-size optimization problem formulation[1]
- compression of helical springs example[1]
- compression run[1]
- configuration file entries and format[1]
- configuration file location[1]
- configuration file - memory handling[1]
- conjugate heat transfer analysis (TFSI) of inline-4 engine head[1]
- CONM1 -[1]
- CONM2 -[1]
- CONNECT -[1]
- connecting rod of a slider crank example - optimization with ESLM[1]
- connectivity - parts and instances[1]
- CONROD -[1]
- constraints ball joint[1]
- constraints constant velocity joint[1]
- constraint screening - gradient-based optimization[1]
- constraints cylindrical joint[1]
- constraints - MBD[1]
- constraints on grids in the design region[1]
- constraints planar joint[1]
- constraints revolute joint[1]
- constraints translational joint[1]
- constraints universal joint[1]
- CONTACT -[1]
- contact analysis output[1]
- contact-based thermal analysis[1]
- contact discretization[1]
- contact discretization - node-to-surface[1]
- contact - friction[1]
- contact - friction models[1]
- contact implementation[1]
- contact interface parameters[1]
- contact interface types[1]
- contact - Lagrange multipliers[1]
- contact - lattice structure optimization[1]
- contact - MBD[1]
- contact - node-to-node discretization[1]
- contact pressure response example[1]
- contact smoothing with two concentric rings[1]
- contact - surface-to-surface discretization[1]
- CONTF -[1]
- continuum shell composites using PCOMPLS[1]
- continuum shells analysis - analysis of composites[1]
- continuum shells - composite laminates[1]
- CONTPRM -[1]
- control of used memory[1]
- CONTX11 -[1]
- CONV -[1]
- convergence considerations for small displacement nonlinear analysis[1]
- convergence enhancement for ESLM[1]
- CORD1C -[1]
- CORD1R -[1]
- CORD1S -[1]
- CORD2C -[1]
- CORD2R -[1]
- CORD2S -[1]
- CORD3R -[1]
- CORD4R -[1]
- coupled frequency response analysis of fluid-structure models[1]
- coupled FRF analysis on a fluid-structure model[1]
- coupled thermal-structural analysis[1]
- coupled thermal structural analysis and optimization[1]
- coupled thermal-structural analysis - nonlinear transient heat transfer[1]
- coupled thermal structure analysis - powertrain applications[1]
- COUPLER -[1]
- CPENTA -[1]
- CPENTA element checks and default bound values[1]
- CPYRA -[1]
- CPYRA element checks and default bound values[1]
- CQAXI -[1]
- CQPSTN -[1]
- CQUAD4 -[1]
- CQUAD4 element checks and default bound values[1]
- CQUAD8 -[1]
- CQUAD8 element checks and default bound values[1]
- CQUADR -[1]
- Craig Bamptom nodal method (CBDN)[1]
- Craig-Bampton method - flexible body generation[1]
- Craig-Chang method - flexible body generation[1]
- critical plane approach[1]
- critical time step - nonlinear explicit analysis[1]
- CROD -[1]
- cross-section optimization of a spot welded tube example[1]
- CSEAM -[1]
- CSEC2 -[1]
- CSEC3 -[1]
- CSEC4 -[1]
- CSEC6 -[1]
- CSEC8 -[1]
- CSET1 -[1]
- CSET -[1]
- CSHEAR -[1]
- CSTRAIN -[1]
- CSTRESS -[1]
- CSUPEXT -[1]
- CTAXI -[1]
- CTAXI / CTRIAX6 element checks and default bound values[1]
- CTETRA -[1]
- CTETRA element checks and default bound values[1]
- CTPSTN -[1]
- CTRIA3 -[1]
- CTRIA3 element checks and default bound values[1]
- CTRIA6 -[1]
- CTRIA6 element checks and default bound values[1]
- CTRIAR -[1]
- CTRIAX6 -[1]
- CTUBE -[1]
- curved cantilever beam verification problem[1]
- CVISC -[1]
- CWELD -[1]
- cyclical pattern grouping[1]
- cylinder shell patch (test no. LE2[1]
- cylindrical pattern grouping[1]
- D
- DAMAGE -[1]
- damage model method - cohesive zone modeling[1]
- Dang Van criterion[1]
- Dang Van fatique optimization example[1]
- DAREA -[1]
- DCOMP -[1]
- DCONADD -[1]
- DCONSTR -[1]
- DDVAL -[1]
- DEBUG -[1]
- debugging guide[1]
- deep simply-supported beam (Test No. FV5)[1]
- defaults summary -[1]
- define free-shape design regions[1]
- definition file - external fluid-structure coupling[1]
- DEFORM -[1]
- DEFORM - subcase information entry[1]
- DELAY -[1]
- DENSITY -[1]
- DENSRES -[1]
- DEQATN -[1]
- DESGLB -[1]
- DESHIS -[1]
- design characterists of topology and free-size[1]
- design interpretation - OSSmooth[1]
- design objective for system identification[1]
- design optimization - aerospace[1]
- design sensitivity analysis example[1]
- design variables for size (parameter) optimization[1]
- design variables for topography optimization[1]
- design variables - topology optimization[1]
- DESOBJ - subcase information entry[1]
- DESSUB - subcase information entry[1]
- DESVAR -[1]
- DESVARG -[1]
- DESVAR - subcase information entry[1]
- DGLOBAL -[1][2]
- diagnosing non-converged solution using NLMON example[1]
- DIM -[1]
- direct frequency response analysis[1]
- direct matrix input (superelements)[1]
- direct matrix input for Finite Element Analysis (superelements)[1]
- direct solvers[1]
- direct transient response - rotor dynamics example[1]
- DISPLACEMENT -[1]
- displacement-based damage index - damage model method[1]
- displacement punch file[1]
- displacement punch file - complex eigenvalue analysis[1]
- displacement punch file - frequency response analysis[1]
- displacement punch file - linear and nonlinear static analysis[1]
- displacement punch file - linear buckling analysis[1]
- displacement punch file - linear transient analysis[1]
- displacement punch file - normal modes analysis[1]
- displacement punch file - random response analysis[1]
- displacement punch file - response spectrum analysis[1]
- displacements - results of finite element analysis[1]
- dlattice -[1]
- DLINK1 -[1]
- DLINK2 -[1]
- DLINK -[1]
- DLOAD -[1]
- DLOAD - subcase information entry[1]
- DMGEVO -[1]
- DMGINI -[1]
- DMIG -[1]
- DMIGMOD -[1]
- DMIGNAME -[1]
- DMIGROT -[1]
- DMVREL: types -[1]
- DOBJREF -[1]
- domain decomposition method (DDM)[1]
- DOPTPRM -[1]
- DOPTPRM, APPROX -[1]
- DOPTPRM, BARCON -[1]
- DOPTPRM, BKLOCAL1 -[1]
- DOPTPRM, BKLOCAL2 -[1]
- DOPTPRM, CHECKER -[1]
- DOPTPRM, CONTOL -[1]
- DOPTPRM, DDVOPT -[1]
- DOPTPRM, DELSHP -[1]
- DOPTPRM, DELSIZ -[1]
- DOPTPRM, DELTOP -[1]
- DOPTPRM, DESMAX -[1]
- DOPTPRM, DISCRETE -[1]
- DOPTPRM, DISCRT1D -[1]
- DOPTPRM, ESLMAX -[1]
- DOPTPRM, ESLSOPT -[1]
- DOPTPRM, ESLSTOL -[1]
- DOPTPRM, GBUCK -[1]
- DOPTPRM, LATLB -[1]
- DOPTPRM, LATTICE -[1]
- DOPTPRM, MATINIT -[1]
- DOPTPRM, MAX_BUCK -[1]
- DOPTPRM, MAXITER -[1]
- DOPTPRM, MINDENS -[1]
- DOPTPRM, MINDIM -[1]
- DOPTPRM, MINMETH -[1]
- DOPTPRM, MMCHECK -[1]
- DOPTPRM, NESLEXPD -[1]
- DOPTPRM, OBJTOL -[1]
- DOPTPRM, OLDPEN -[1]
- DOPTPRM, OPTIMOMP - bulk data entry[1]
- DOPTPRM, OPTMETH -[1]
- DOPTPRM, PNORM -[1]
- DOPTPRM, POROSITY -[1]
- DOPTPRM, REMESH -[1]
- DOPTPRM, SHAPEOPT -[1]
- DOPTPRM, TMINPLY -[1]
- DOPTPRM, TOPDISC -[1]
- DOPTPRM, TOPDV -[1]
- DOPTPRM, TOPRST -[1]
- DPHASE -[1]
- DRAPE -[1]
- draw direction constraint - free-shape optimization[1]
- draw direction constraints - topology optimization[1]
- DREPADD -[1]
- DREPORT -[1]
- DRESP1 -[1]
- DRESP1 - center of gravity and moments of inertia item codes[1]
- DRESP1 - composite static failure item codes[1]
- DRESP1 - contact force response item codes[1]
- DRESP1 - frequency response displacement, velocity, and acceleration item codes[1]
- DRESP1 - frequency response force item codes[1]
- DRESP1 - frequency response pressure item codes[1]
- DRESP1 - frequency response stress/strain item codes[1]
- DRESP1 - MBD displacement item codes[1]
- DRESP1 - MBD force item codes[1]
- DRESP1 - MBD velocity/acceleration item codes[1]
- DRESP1 - PSD/RMS displacement, velocity, and acceleration item codes[1]
- DRESP1 - PSD/RMS pressure item codes[1]
- DRESP1 - PSD/RMS stress/strain item codes[1]
- DRESP1 - responses and attributes[1]
- DRESP1 - section property item codes[1]
- DRESP1 - static failure item codes[1]
- DRESP1 - static force item codes[1]
- DRESP1 - static stress/strain item codes[1]
- DRESP1 - static stress/strain item codes for composites[1]
- DRESP1 - static stress item codes for bar elements using PBARL, PBEAML properties[1]
- DRESP2 -[1]
- DRESP3 -[1]
- DRESPONSE -[1]
- DSA -[1]
- DSCREEN -[1]
- DSHAPE -[1]
- DSHUFFLE -[1]
- DSIZE -[1]
- DSYSID -[1]
- DTABLE -[1]
- DTI,SPECSEL -[1]
- DTI,UNITS -[1]
- DTPG -[1]
- DTPL -[1]
- DVCREL1 -[1]
- DVCREL2 -[1]
- DVCREL: types -[1]
- DVGRID -[1]
- DVLREL1 -[1]
- DVLREL2 -[1]
- DVMBRL1 -[1]
- DVMBRL2 -[1]
- DVMREL1 -[1]
- DVMREL2 -[1]
- DVPREL1 -[1]
- DVPREL2 -[1]
- DVPREL: Types -[1]
- dynamic/nonlinear analysis - internal responses[1]
- dynamic analysis - debug methods[1]
- dynamic behavior of fluid-containing structure using MFLUID example[1]
- dynamic condensation[1]
- E
- ECHO -[1]
- ECHOOFF -[1]
- ECHOON -[1]
- EDE -[1]
- EDGEBH -[1]
- EDRAWB -[1]
- EIGC -[1]
- eigenvalue maximization with topography optimization[1]
- eigenvalue solvers[1]
- eigenvector orthonormalization[1]
- EIGRA -[1]
- EIGRD -[1]
- EIGRL -[1]
- EIGVNAME -[1]
- EIGVRETRIEVE - subcase information entry[1]
- EIGVSAVE - subcase information entry[1]
- EKE -[1]
- EL2PROP -[1]
- elastic, damper and mass elements[1]
- elastic-plastic large displacement analysis[1]
- element quality check[1]
- element results representation for models[1]
- elements[1]
- elements - non-structural mass[1]
- ELEMQUAL -[1]
- ELFORCE -[1]
- ELIST -[1]
- elliptic membrane (test no. LE1)[1]
- ELSM - convergence enhancement[1]
- ELSTRESS -[1]
- E-N approach - fatigue analysis[1]
- E-N approach - multiaxial fatigue analysis[1]
- END -[1]
- ENDLOAD -[1]
- ENERGY -[1]
- energy dissipation-based damage index - damage model method[1]
- enhance the design process[1]
- environment variables[1]
- EQSTSAMP -[1]
- equivalent static load - displacement[1]
- equivalent static load method (ESLM)[1]
- ERP -[1]
- ERPPNL -[1]
- error message database[1]
- Error Messages[1][2][3][4][5]
- ESE -[1]
- ESLM example - MBD system level response optimization[1]
- ESLM for MBD[1]
- ESLM for MBD method[1]
- ESLM for nonlinear response optimization[1]
- ESLM output requests[1]
- ESLM parameters[1]
- ESLM parameters MBD[1]
- ESLTADD -[1]
- ESLTIME -[1]
- ESLTIME - subcase information entry[1]
- example, manifold: nonlinear transient heat transfer[1]
- example cantilever beam using equations - size (parameter) optimization[1]
- example - direct matrix input for finite element analysis (superelements)[1]
- example problems for shape optimization[1]
- example shell cantilever - size optimization[1]
- examples - symbolic substitution[1]
- example ten bar truss - size (parameter) optimization[1]
- EXCLUDE - subcase information entry[1]
- expanded error message file[1]
- expanded error message file location[1]
- explicit analysis time step parameters[1]
- explicit dynamic analysis - beta release[1]
- explicit dynamic analysis - loads and boundary conditions[1]
- explicit dynamic analysis - problem setup[1]
- explicit dynamic analysis - solution method[1]
- explicit dynamic analysis - user's consideration[1]
- explicit finite element analysis method[1]
- external acoustic using infinite element method - hi-tech electronic applications[1]
- external acoustic using RADSND method - hi-tech electronic applications[1]
- external fluid-structure coupling definition file[1]
- external optimization responses (DRESP3) example[1]
- external responses[1][2]
- external responses using solidThinking Compose[1]
- extrusion constraint - free-shape optimization[1]
- extrusion constraints - topology optimization manufacturability[1]
- F
- factor of safety - Dang Van Criterion[1]
- failsafe topology optimization[1]
- failsafe topology optimization of 3D column[1]
- FAILURE -[1]
- failure criteria - composite continuum shells[1]
- failure criteria - composite laminated shells[1]
- failure evaluation - seam weld fatigue analysis[1]
- faq - optimization setup[1]
- faq - post-processing and results output[1]
- faq - SPMD: DDM[1]
- FASTFR - solvers[1]
- FastFRS - solvers[1]
- FATDEF -[1]
- FATDEF - subcase information entry[1]
- FATEVNT -[1]
- fatigue analysis[1]
- fatigue analysis - output for third party software[1]
- fatigue analysis - powertrain applications[1]
- fatigue analysis setup[1]
- fatigue analysis tutorials[1]
- fatigue - internal responses[1]
- fatigue properties - seam weld analysis[1]
- FATLOAD -[1]
- FATMCRV -[1]
- FATPARM -[1]
- FATPARM - subcase information entry[1]
- FATSEAM -[1]
- FATSEQ -[1]
- FATSEQ - subcase information entry[1]
- FE analysis - defaults[1]
- FEA solution with pretensioning[1]
- FEA solution with pretensioning - 1D bolt[1]
- FEA solution with pretensioning - 3D bolt[1]
- FEA topography for reanalysis[1]
- FEA topology for reanalysis[1]
- features - optimization[1]
- Features - Shape Optimization[1]
- features - size (parameter) optimization[1]
- Features - Structural Optimization in Multibody Dynamics Systems[1]
- FEM - aerospace[1]
- file location - configuration file[1]
- file names, headers, and locations default[1]
- file output controls[1]
- finite element analysis[1]
- finite element analysis results[1]
- finite element model validation - aerospace[1]
- finite sliding contact example[1]
- FLDATA -[1]
- flexible body generation[1]
- Flexible Body Generation Input/Output[1]
- FLLWER -[1]
- FLLWER - subcase information entry[1]
- FLSPOUT -[1]
- fluid-structure interaction[1]
- fluid structure interaction analysis[1]
- fluid structure interaction input[1]
- Fluid Structure Interaction Output[1]
- fluid structure interaction - workflow[1]
- fluid-structure interface[1]
- fluid-structure interface visualization and refinement[1]
- FLUX -[1]
- Flux OptiStruct[1]
- foldable phone analysis - hi-tech electronic applications[1]
- FORCE1 -[1]
- FORCE2 -[1]
- FORCE -[1][2]
- force punch file[1]
- force punch file - frequency response analysis[1]
- forge a design concept out of a solid block example[1]
- FORMAT -[1][2]
- formats[1]
- forward creep at steady twist rate - verification[1]
- FOS -[1]
- fourier transformation - linear transient analysis[1]
- free cylinder: axi-symmetric vibration (test no. FV41)[1]
- free-shape design regions - define[1]
- free-shape optimization[1]
- Free-shape Optimization - Features[1]
- free-shape parameters[1]
- free-size optimization[1]
- Free-size Optimization - Features[1]
- free-size optimization member size control[1]
- free-size optimization - pattern grouping[1]
- free-size pattern repetitiion[1]
- free-sizing optimization - manufacturability[1]
- free thin square plate (Test No. FV12)[1]
- FREQ1 -[1]
- FREQ2 -[1]
- FREQ3 -[1]
- FREQ4 -[1]
- FREQ5 -[1]
- FREQ -[1]
- frequency response analysis[1]
- frequency response analysis - hi-tech electronic applications[1]
- frequency response analysis - MPCFORCE[1]
- frequency response analysis of 3D rotor dynamics model[1]
- frequency response function - internal responses[1]
- frequency response loadcases[1][2]
- frequency response loads and boundary conditions[1]
- FREQUENCY - subcase information entry[1]
- FRF analysis[1]
- friction - contact[1]
- friction models - contact[1]
- FSI -[1]
- FSI - subcase information entry[1]
- fully-qualified references - parts and instances[1]
- function expressions - MBD[1]
- G
- GAPPRM -[1]
- GAPPRM, CHKRUN[1]
- GAPPRM, CKGPDIR[1]
- GAPPRM, ERRMSG[1]
- GAPPRM, GAPCMPL[1]
- GAPPRM, GAPGPRJ[1]
- GAPPRM, GAPOFFS[1]
- GAPPRM, GPCOINC[1]
- GAPPRM, HMGAPST[1]
- GAPPRM, PRTSW[1]
- Gasket and Engine Block System Connected Using Head Bolts[1][2]
- GENEL -[1]
- general acceleration PCH format - punch file[1]
- general - create output for third party software[1]
- general displacement PCH format - punch file[1]
- general element force pch format - punch file[1]
- general method (GM)[1]
- general MPCFORCE PCH format - punch file[1]
- general output information[1]
- general stress PCH format - punch file[1]
- general velocity PCH format - punch file[1]
- generate and evaluate a design using topology optimization[1]
- generate the matrices[1]
- global-local modeling[1]
- global-local modeling - subcase specific[1]
- global search option - design optimization[1]
- global search option NVH[1]
- GLOBSUB - subcase information entry[1]
- GMATCH -[1]
- governing equations - normal modes analysis[1]
- governing equations - random spectrum analysis[1]
- GPFORCE -[1]
- GPFOS -[1]
- GPKE -[1]
- GPSTRAIN -[1]
- GPSTRESS / GSTRESS -[1]
- gradient-based optimization method[1]
- gradient-based optimization - regular or soft convergence[1]
- graphics processing unit[1]
- GRAV -[1]
- GRDSET -[1]
- GRID -[1]
- grid point stresses - results of a finite element analysis[1]
- grid point stress response for free-shape optimization[1]
- GRIDS -[1]
- GROUND -[1]
- GROUNDCHECK - subcase information entry[1]
- GSO - global search option[1]
- GT-SUITE[1]
- guidelines[1]
- H
- hardware - OptiStruct[1]
- hardware recommendations[1]
- heat flux loads - apply[1][2]
- heat transfer analysis - internal responses[1]
- HISOUT -[1]
- hi-tech electronic applications - User Guide[1]
- hoe normal offset of 3-node edge[1]
- hoe tangent offset of 3-node edge[1]
- hot spot stress - seam weld fatigue analysis[1]
- hourglass control[1]
- hourglass control parameters[1]
- HOURGLS -[1]
- HYBDAMP -[1][2]
- hybrid shared/distribution memory parallelization (SPMD)[1]
- Hyper3D binary file (.h3d)[1]
- hyperelastic material verification[1]
- hyperelastic - pressurized rubber disk[1]
- HyperGraph[1]
- HyperMesh[1][2][3][4][5][6]
- HyperView[1][2][3][4][5][6][7]
- HyperWorks[1]
- I
- I/O options by function[1]
- i/o options section[1]
- IC - subcase information entry[1]
- IDGLOBALIC - subcase information entry[1]
- id resolution guidelines - parts and instances[1]
- IMPERF -[1]
- imperfection[1]
- IMPERF - subcase information entry[1]
- implementation SMP[1]
- IMPORT -[1]
- INCLUDE -[1][2]
- inertia relief[1]
- INFILE -[1]
- INISTRS -[1]
- INISTRS - subcase information entry[1]
- initial velocity - MBD[1]
- input data[1]
- input data - thermal structural analysis[1]
- input - linear transient analysis by fourier transformation[1]
- input - random response fatigue analysis[1]
- input - sine sweep fatigue analysis[1]
- input specification - response spectrum analysis[1]
- input specifications - normal modes analysis[1]
- INSTANCE -[1]
- instances - parts and instances[1]
- INSTNCE -[1]
- internal response - OptiStruct[1]
- internal responses[1]
- internal superelements[1]
- interpretation of results for composites[1]
- interpretation of topogrpahy optimziation results[1]
- interpretation of topology optimization results[1]
- interpret free-size results[1]
- interpret topology and free-size results[1]
- introductory example shape optimization[1]
- INVELB -[1]
- INVELJ -[1]
- INVEL - subcase information entry[1]
- ISTSADD -[1]
- iterative solution - gradient-based optimization[1]
- iterative solvers[1]
- J
- K
- K2GGIC - subcase information entry[1]
- K2PP - subcase information entry[1]
- K42GG - subcase information entry[1]
- keywords - symbolic substitution[1]
- L
- LABEL - subcase information entry[1]
- Lagrange multipliers (MPC-based)[1]
- laminated shell strength analysis - mechanical load 1[1]
- laminated shell strength analysis - mechanical load 2[1]
- laminated shell strength analysis - mechanical load 3[1]
- laminated shell strength analysis - thermal load 1[1]
- laminated strip[1]
- Lanczos - Solvers[1]
- Laplacian smoothing[1]
- large displacement analysis of chassis[1]
- Large Displacement FEA Tutorials[1]
- Large Displacement FEA Tutorials OptiStruct[1]
- large displacement subcase example[1]
- large number of design variables - MBD system level response optimization[1]
- large scale optimization algorith (BIGOPT)[1]
- large shape change optimization[1]
- laser edge overlap - seam weld fatigue analysis[1]
- LATPRM -[1]
- LATPRM, BOUNDARY -[1]
- LATPRM, BUCKSF -[1]
- LATPRM, CLEAN -[1]
- LATPRM, LATLB -[1]
- LATPRM, LATSUP -[1]
- LATPRM, LATTICE -[1]
- LATPRM, MAXRAD -[1]
- LATPRM, MINRAD -[1]
- LATPRM, ONEDVPGR -[1]
- LATPRM, OSSRMSH -[1]
- LATPRM, POROSITY -[1]
- LATPRM, R2LRATIO -[1]
- LATPRM, STRMETH -[1]
- LATPRM, TETSPLT -[1]
- lattice generation (phase 1) - lattice structure optimization[1]
- lattice sizing+ - lattice structure optimization[1]
- lattice structure optimization[1]
- lattice structure optimization, example[1]
- lattice structure optimization - automated reanalysis[1]
- lattice structure optimization - compliance management[1]
- lattice structure optimization - contact[1]
- lattice structure optimization - size (parameter) optimization (phase 2)[1]
- lattice structure optimization - smoothing and remeshing[1]
- lattice structure optimization - stiffness penalization[1]
- lattice structure optimization - stress constraints[1]
- lattice structure optimizatio - porosity control[1]
- launch FSO[1]
- launch mmo[1]
- level set method (Beta)[1]
- level-set optimization setup[1]
- LIFE -[1]
- limitations - MBD system level response optimization[1]
- LINE -[1]
- linear analysis - MBD[1]
- linear buckling analysis[1]
- linear buckling analysis - internal responses[1]
- linear direct transient response[1]
- linear modal transient response[1]
- linear penalty curve (nonlinear analysis[1]
- linear static analysis[1]
- linear static analysis - rotor dynamics example[1]
- linear steady-state heat transfer analysis[1]
- linear transient analysis[1]
- linear transient analysis by fourier transformation[1]
- linear transient analysis by fourier transformation - displacement[1]
- linear transient analysis by Fourier Transformation - velocity punch file[1]
- linear transient analysis - internal responses[1]
- linear transient heat transfer analysis[1]
- Linux[1]
- LOAD -[1]
- LOADADD -[1]
- LOADJG -[1]
- LOADJG - subcase information entry[1]
- LOADLIB -[1]
- Load on Flexible Body[1]
- loads and boundary conditions[1]
- loads on the fluid mesh - coupled frequency response analysis by fourier[1]
- LOAD - subcase information entry[1]
- load time history compression[1]
- local and global entries - parts and instances[1]
- local coordinate systems for JOINTG[1]
- LOCATE -[1]
- LOCATE - subcase information entry[1]
- M
- M2GG - subcase information entry[1]
- manufacturability for free-sizing optimization[1]
- manufacturability for topography optimization[1]
- manufacturability for topology optimization[1]
- manufacturing constraints[1]
- MARKER -[1]
- markers - MBD[1]
- mass elements[1]
- MASSTOH3D -[1]
- MASTA[1]
- MAT1 -[1]
- MAT2 -[1]
- MAT3 -[1]
- MAT4 -[1]
- MAT5 -[1]
- MAT8 -[1]
- MAT9 -[1]
- MAT9OR -[1]
- MAT10 -[1]
- material property check[1]
- material property checks for MAT1[1]
- material property checks for MAT2[1]
- material property checks for MAT3[1]
- material property checks for MAT8[1]
- material property checks for MAT9[1]
- materials[1]
- MATF1 -[1]
- MATF2 -[1]
- MATF3 -[1]
- MATF8 -[1]
- MATF9 -[1]
- MATF10 -[1]
- MATF -[1]
- MATFAT -[1]
- MATHE -[1]
- MATHF -[1]
- MATMDS -[1]
- MATPE1 -[1]
- matrices in a finite element analysis[1]
- MATS1 -[1]
- MATT1 -[1]
- MATT2 -[1]
- MATT3 -[1]
- MATT4 -[1]
- MATT8 -[1]
- MATT9 -[1]
- MATT9OR -[1]
- MATTVP -[1]
- MATUSR -[1]
- MATVE -[1]
- MATVP -[1]
- MATX0 -[1]
- MATX02 -[1]
- MATX13 -[1]
- MATX21 -[1]
- MATX25 -[1]
- MATX27 -[1]
- MATX28 -[1]
- MATX33 -[1]
- MATX36 -[1]
- MATX38 -[1]
- MATX42 -[1]
- MATX43 -[1]
- MATX44 -[1]
- MATX60 -[1]
- MATX62 -[1]
- MATX65 -[1]
- MATX68 -[1]
- MATX70 -[1]
- MATX82 -[1]
- Maximum Bead Width Constrain for Topology Optimization of Oil Pan[1]
- maximum member size control[1]
- MAXMIN - subcase information entry[1]
- MBACT -[1]
- MBCNTDS -[1]
- MBCNTR -[1]
- MBCRV -[1]
- MBCVCV -[1]
- MBDCRV -[1]
- MBDEACT -[1]
- MBD - ESLM[1]
- MBD parameters for ESLM[1]
- MBDSRF -[1]
- MBD system level response optimization[1]
- MBFORCE -[1]
- MBFRC -[1]
- MBFRCC -[1]
- MBFRCE -[1]
- MBLIN -[1]
- MBMNT -[1]
- MBMNTC -[1]
- MBMNTE -[1]
- MBPCRV -[1]
- MBPTCV -[1]
- MBPTDCV -[1]
- MBPTDSF -[1]
- MBREQ -[1]
- MBREQE -[1]
- MBREQM -[1]
- MBSEQ -[1]
- MBSFRC -[1]
- MBSFRCC -[1]
- MBSFRCE -[1]
- MBSIM -[1]
- MBSIMP -[1]
- MBSIM - subcase information entry[1]
- MBSMNT -[1]
- MBSMNTC -[1]
- MBSMNTE -[1]
- MBVAR -[1]
- MCOHE -[1]
- MCOHED -[1]
- MDSDIR -[1]
- measure sound ration from impacting plates example[1]
- MECHCHECK -[1]
- member size control for topology optimization[1]
- member size control - free-size optimization[1]
- member size control - maximum member size control[1]
- member size control - minimum member size control[1]
- membrane with hot-spot (test no. T1)[1]
- memory allocation[1]
- memory handling - control of used memory[1]
- memory limitation - virtual vs physical memory[1]
- memory - solvers[1]
- mesh barrier constraints - free-shape optimization[1]
- METADATA -[1]
- METHOD - subcase information entry[1]
- MFLUID -[1]
- MFLUID - subcase information entry[1]
- MGASK -[1]
- microphone location - radiated sound output analysis[1]
- Microsoft Excel example - external responses[1]
- minimize objective function - design optimization[1]
- minimum member size control[1]
- minmax objective function - design optimization[1]
- MINMAX - subcase information entry[1]
- miscellaneous - defaults[1]
- MLOAD -[1]
- MLOAD - subcase information entry[1]
- modal and panel participation - coupled frequency response analysis by fourier[1]
- modal complex eigenvalue analysis - rotor dynamics example[1]
- MODALDE -[1]
- modal frequency response analysis[1]
- modal frequency response analysis output[1]
- MODALKE -[1]
- modal participation example[1]
- MODALSE -[1]
- modal transient response output[1]
- MODCHG -[1]
- MODCHG - subcase information entry[1]
- MODEL -[1]
- model guidelines - rotor dynamics[1]
- modeling errors - rigid body modes[1]
- modeling techniques[1]
- modeling techniques - cohesive zone modeling[1]
- MODELMPC - subcase information entry[1]
- MODESELECT - subcase information entry[1]
- MODEWEIGHT - subcase information entry[1]
- MODOUT -[1]
- MODTRAK - subcase information entry[1]
- MOMENT1 -[1]
- MOMENT2 -[1]
- MOMENT -[1]
- MONITOR -[1]
- monitor nonlinear structural analysis and structural FSI[1]
- MONITOR - subcase information entry[1]
- MOTION -[1]
- MotionSolve[1]
- MOTION - subcase information entry[1]
- MOTNG -[1]
- MOTNGC -[1]
- MOTNGE -[1]
- MOTNJ -[1]
- MOTNJC -[1]
- MOTNJE -[1]
- MOTNJG -[1]
- MOTNJG - subcase information entry[1]
- move limit adjustments - gradient-based optimization[1]
- MPC -[1]
- MPCADD -[1]
- MPCFORCE -[1]
- MPC - subcase information entry[1]
- MPI, DDM and MMO problems - debug methods[1]
- MSGLMT -[1]
- multiaxial fatigue analysis[1]
- multiaxial fatigue analysis - .rnf file[1]
- multibody dynamic analysis[1]
- multibody dynamics analysis - internal responses[1]
- multibody dynamics analysis tutorials[1]
- multibody dynamics features[1]
- multibody dynamics simulation[1]
- multi-dimensional table[1]
- multi-model optimization (MMO)[1]
- multi-model optimization (MMO) – design scaling with pattern-repetition in two different C-clips[1]
- multi-model optimization (MMO) – pattern repetition of an excavator arm[1]
- multi-plane symmetric reinforcement optimization for a pressure vessel example[1]
- multiple rotors - rotor dynamics[1]
- multipoint constraint force - punch file[1]
- multiscale modeling[1]
- multiscale model - MDS modeling[1]
- multiscale results - MDS modeling[1]
- MUMPS - solvers[1]
- N
- N2S contact-based fast contact[1]
- NAFEMS composite benchmark problems[1]
- NAFEMS free vibration problems[1]
- NAFEMS heat transfer problem[1]
- NAFEMS linear elastic problems[1]
- NAFEMS Test 5H – Deep Simply-Supported Beam Harmonic Forced Vibration Response[1]
- NAFEMS Test 5P – Deep Simply-Supported Beam Periodic Forced Vibration Response[1]
- NAFEMS Test 5R – Deep Simply-Supported Beam Random Forced Vibration Response[1]
- NAFEMS Test 5T – Deep Simply-Supported Beam Transient Forced Vibration Response[1]
- NAFEMS Test 13H – Simply-Supported Thin Square Plate Harmonic Forced Vibration Response[1]
- NAFEMS Test 13P – Simply-Supported Thin Square Plate Periodic Forced Vibration Response[1]
- NAFEMS Test 13R – Simply-Supported Thin Square Plate Harmonic Forced Vibration Response[1]
- NAFEMS Test 13T – Simply-Supported Thin Square Plate Transient Forced Vibration Response[1]
- NAFEMS Test 21H – Simply-Supported Thick Square Plate Harmonic Forced Vibration Response[1]
- NAFEMS Test 21P – Simply-Supported Thick Square Plate Periodic Forced Vibration Response[1]
- NAFEMS Test 21R – Simply-Supported Thick Square Plate Random Forced Vibration Response[1]
- NAFEMS Test 21 – Simply-Supported Thick Square Plate[1]
- NAFEMS Test 21T – Simply-Supported Thick Square Plate Transient Forced Vibration Response[1]
- NAFEMS Test No. 13 – simply-supported thin square plate[1]
- nafems test no. FV41 - free cylinder: axi-symmetric vibration[1]
- nafems test no. LE5 - Z-section cantilever[1]
- nafems test no. LE6 - skew plate normal pressure[1]
- nafems test no. LE10 -thick plate pressure[1]
- nafems test no. LE11 - solid cylinder/taper/sphere - temperature[1]
- nafems test no. T1 - membrane with hot-spot[1]
- nafems test no. T4 - two-dimensional heat transfer with convection[1]
- NAFEMS test problem (LE3) - radial point load[1]
- NAFEMS thermo-elastic problems[1]
- NAFEMS Vibrating Cylinder[1]
- NAFEMS Vibrating Sphere[1]
- Nastran[1][2][3][4][5][6]
- nastran punch file (.pch)[1]
- NLADAPT -[1]
- NLADAPT - subcase information entry[1]
- NLLOAD -[1]
- NLMON -[1]
- NLMON - subcase information entry[1]
- NLOAD1 -[1]
- NLOAD -[1]
- NLOAD - subcase information entry[1]
- NLOUT -[1]
- NLOUT - subcase information entry[1]
- NLPARM -[1]
- NLPARM - subcase information entry[1]
- NLPCI -[1]
- NLRESTART -[1]
- NLRGAP -[1]
- node-to-node discretization[1]
- node-to-surface discretization[1]
- noise vibration and harshness (NVH) analysis - powertrain applications[1]
- NOISEXYZ -[1]
- NOLIN1 -[1]
- NOLIN2 -[1]
- NOLIN3 -[1]
- NOLIN4 -[1]
- nonlinar transient thermal subcase continuation[1]
- Nonlinear Adaptive Criteria and Nonlinear Intermediate Results[1]
- nonlinear analysis of cantilever beam example[1]
- nonlinear analysis of cantilever beams with follower forces[1]
- nonlinear analysis of inline-4 engine head example[1]
- nonlinear analysis of rack and pinion using restart[1]
- nonlinear analysis static of wheel rail interface using fast contact[1]
- nonlinear convergence criteria[1]
- nonlinear direct transient analysis problem setup[1]
- nonlinear explicit analysis problem setup[1]
- nonlinear implicit analysis[1]
- nonlinearity sources - nonlinear direct transient analysis[1]
- nonlinearity sources - nonlinear explicit analysis[1]
- nonlinearity sources - nonlinear static analysis[1]
- nonlinear larg displacement analysis examples[1]
- nonlinear optimization monitoring[1]
- nonlinear penalty curve (nonlinear analysis)[1]
- nonlinear small displacement analysis examples[1]
- nonlinear solution method[1]
- nonlinear static (large displacement) analysis of snap fit assembly using continuous sliding example[1]
- nonlinear static analysis[1]
- nonlinear static analysis - debug methods[1]
- nonlinear static analysis - powertrain applications[1]
- nonlinear static analysis problem setup[1]
- nonlinear static analysis types[1]
- nonlinear static analysis with contacts and pretensioning of bolts example[1]
- nonlinear static analysis with hyperelastic material model, under compression loading and unloading example[1]
- nonlinear steady-state heat transfer analysis[1]
- nonlinear steady-state heat transfer - powertrain applications[1]
- nonlinear structural analysis - monitor[1]
- NONLINEAR - subcase information entry[1]
- nonlinear transient analysis[1]
- nonlinear transient heat transfer analysis (Beta)[1]
- nonlinear transient heat transfer analysis - input[1]
- non-reflecting boundary - coupled frequency response analysis by fourier[1]
- non-structural mass elements[1]
- normal modes analysis[1]
- normal modes analysis - governing equations[1]
- normal modes analysis - hi-tech electronic applications[1]
- normal modes analysis - internal responses[1]
- normal modes analysis of a compressor wheel example[1]
- normal modes analysis output[1]
- normal modes with pre-load analysis of chair frame[1]
- NORM - subcase information entry[1]
- no symmetry[1]
- NSGE1 -[1]
- NSGE -[1]
- NSGEADD -[1]
- NSGE - subcase information entry[1]
- NSM1 -[1]
- NSM -[1]
- NSMADD -[1]
- NSML1 -[1]
- NSML -[1]
- NSM - subcase information entry[1]
- NVH applications and techniques[1]
- O
- offset elements - buckling analysis[1]
- OFREQUENCY -[1]
- OLOAD -[1]
- OMODES -[1]
- one dimensional transient heat transfer (test no. T3)[1]
- one plane - simple symmetry options[1]
- one step thermal transient stress analysis, example[1]
- one step transient thermal stress analysis[1]
- one step transient thermal stress optimization[1]
- optimizaiton problems - debug methods[1]
- optimization - defaults[1]
- optimization - features[1]
- optimization of a cantilever beam modeled with solid elements[1]
- optimization of arbitrary beam sections[1]
- optimization of a two-layer stamped control arm[1]
- optimization of composite structures[1]
- optimization of MBD system level response optimization example[1]
- optimization of the modal frequencies of a disc using constrained beading patterns example[1]
- optimization of thin-walled sections - arbitrary beam[1]
- optimization output - defaults[1]
- optimization output files[1]
- optimization output - OUTPUT[1]
- optimization process[1]
- optimization setup - faq[1]
- optimization shape[1]
- optimization size (parameter)[1]
- optimization topography[1]
- optimization topology[1]
- optimization using compose function[1]
- optimization with ESLM - connecting rod of a slider crank example[1]
- optimization with ESLM example problems[1]
- optimization with ESLM - rotating bar example[1]
- optimization with ESLM - rotating shell example[1]
- OptiStruct[1][2][3][4][5][6][7][8][9][10][11][12][13][14][15][16][17][18][19][20][21][22][23][24][25][26][27][28][29][30][31][32][33][34][35][36][37][38][39][40][41][42][43][44][45][46][47][48][49][50][51][52][53][54][55][56][57][58][59][60]
- OptiStruct 2020 release notes[1]
- OptiStruct AcuSolve[1]
- OptiStruct HyperMesh[1]
- OptiStruct Linux[1][2]
- OptiStruct reference guide[1]
- OptiStruct tutorials[1]
- OS-E: 0160[1]
- OS-E: 0165[1]
- OS-E: 0170[1]
- OS-E: 0195[1]
- OS-E: 0196 Postbuckling Analysis of Cylinder using Impection[1]
- OS-E: 0895 Flat Plate with Thermal Compliance Response[1]
- OS-E: 0896 Multi-Material Topology Optimization of Automotive Cradle[1]
- OS-E: 0897 Multi-Material Topology Optimization of Automotive Chassis[1]
- OS-E: 5010 High Frequency Electromagnetic and Thermal Analysis of Antenna[1]
- OS-E: 8000 3-Point Bending of Phone[1]
- OS-MBD stress recovery[1]
- OSSmooth input file example[1]
- OSSmooth parameter file[1]
- OSSmooth - running[1]
- OS-T: 1000 Linear Static Analysis of a Plate with a Hole[1]
- OS-T: 1010 Thermal Stress Analysis of a Coffee Pot Lid[1]
- OS-T: 1020 Normal Modes Analysis of a Splash Shield[1]
- OS-T: 1030 3D Inertia Relief Analysis[1]
- OS-T: 1040 3D Buckling Analysis[1]
- OS-T: 1050 Connection of Dissimilar Meshes using CWELD Elements[1]
- OS-T: 1060 Analysis of a Composite Aircraft Structure using PCOMPG[1]
- OS-T: 1070 Analysis of an Axi-symmetric Structure[1]
- OS-T: 1080 Coupled Linear Heat Transfer/Structure Analysis[1][2]
- OS-T: 1085 Linear Steady State Heat Convection Analysis[1]
- OS-T: 1090 Linear Transient Heat Transfer Analysis of an Extended Surface Heat Transfer Fin[1]
- OS-T: 1100 Thermal Stress Analysis of a Printed Circuit Board with Anisotropic Material Properties[1]
- OS-T: 1110 Setting up a Modal Analysis[1]
- OS-T: 1300 Direct Frequency Response Analysis of a Flat Plate[1]
- OS-T: 1305 Modal Frequency Response Analysis of a Flat Plate[1]
- OS-T: 1310 Direct Transient Dynamic Analysis of a Bracket[1]
- OS-T: 1315 Modal Transient Dynamic Analysis of a Bracket[1]
- OS-T: 1320 Nonlinear Gap Analysis of an Airplane Wing Rib[1]
- OS-T: 1325 Random Response Analysis of a Flat Plate[1]
- OS-T: 1330 Acoustic Analysis of a Half Car Model[1]
- OS-T: 1340 Fatigue (Stress - Life) Method[1]
- OS-T: 1340 Fatigue Process Manager (FPM) using S-N (Stress - Life) Method[1]
- OS-T: 1340 Fatigue using S-N (Stress - Life) Method[1]
- OS-T: 1350 Fatigue (Strain - Life) Method[1]
- OS-T: 1350 Fatigue Process Manager (FPM) using E-N (Strain - Life) Method[1]
- OS-T: 1350 Fatigue using E-N (Strain - Life) Method[1]
- OS-T: 1360 NLSTAT Analysis of Gasket Materials in Contact[1][2]
- OS-T: 1365 NLSTAT Analysis of Solid Blocks in Contact[1][2]
- OS-T: 1370 Complex Eigenvalue Analysis of a Reduced Brake System[1]
- OS-T: 1371 Brake Squeal Analysis of Brake Assembly[1]
- OS-T: 1372 Rotor Dynamics of a Hollow Cylindrical Rotor[1]
- OS-T: 1375 Response Spectrum Analysis of a Structure[1]
- OS-T: 1380 Computation of Equivalent Radiated Power[1]
- OS-T: 1385 Heat Transfer Analysis on Piston Rings wth GAP Elements[1]
- OS-T: 1390: 1D and 3D Pretensioned Bolt Analysis of an IC Engine Cylinder Head[1][2]
- OS-T: 1392 Node-to-Surface versus Surface-to-Surface Contact[1][2]
- OS-T: 1393 Basics of Contact Properties and Debugging[1]
- OS-T: 1394 Axi-Symmetric Ball Joint[1]
- OS-T: 1395 acoustic analysis of speaker using RADSND[1]
- OS-T: 1500: bending of plate[1]
- OS-T: 1510 Follower Loads[1]
- OS-T: 1520 Finite Sliding of Rack and Pinion Gear Model[1]
- OS-T: 1530 Bumper Impact[1]
- OS-T: 1540 Compression of Helical Spring using Self-Contact[1]
- OS-T: 1600 Fluid-Structure Interaction Analysis of Piezoelectric Harvester Assembly[1]
- OS-T: 1610 Thermal Fluid-Structure Interaction Analysis on a Manifold[1]
- OS-T: 1900 Dynamic Analysis of a Three-body Model[1]
- OS-T: 1910 Dynamic Analysis of a Slider Crank with a Flexible Connecting Rod[1]
- OS-T: 1920 Large Displacement Analysis of a Cantilever Beam[1]
- OS-T: 1940 MBD Rigid Contact[1]
- OS-T: 1950 Curve to Curve Constraint[1]
- OS-T: 1960 Define Point to Deformable[1]
- OS-T: 2000 Design Concept for a Structural C-Clip[1]
- OS-T: 2005 Design Concept for a Structural C-Clip with Minimum Member Size Control[1]
- OS-T: 2010 Design Concept for an Automotive Control Arm[1]
- OS-T: 2020 Increase Natural Frequencies of an Automotive Splash Shield with Ribs[1]
- OS-T: 2030 Control Arm Topology Optimization with Draw Direction Constraints[1]
- OS-T: 2040 Spot Weld Reduction using CWELD and 1D[1]
- OS-T: 2050 Pattern Repetition using Topology Optimization[1]
- OS-T: 2060 Symmetry and Draw Direction Applied Simultaneously in Topology Optimization[1]
- OS-T: 2070 Topology Optimization of a Reduced Model using DMIG[1]
- OS-T: 2080 Topology Optimization of a Hook with Stress Constraints[1]
- OS-T: 2090 Extrusion Constraints[1]
- OS-T: 2095 Frequency Response Optimization of a Rectangular Plate[1]
- OS-T: 2098 Excavator Arm Model[1]
- OS-T: 3000 Topography Optimization of a Plate Under Torsion[1]
- OS-T: 3010 Topography Optimization of an L-bracket[1]
- OS-T: 3020 Automatic Recognition of Bead Results of an L-bracket[1]
- OS-T: 3030 Random Response Optimization[1]
- OS-T: 3100 Combined Topology and Topography Optimization of a Slider Suspension[1]
- OS-T: 3200 Optimization-driven Design of a Composite Aircraft Underbelly Fairing[1]
- OS-T: 3300 Using the Lattice Optimization Process[1]
- OS-T: 3400 Design an Open Hole Tension (OHT)[1]
- OS-T: 4000 3D Size Optimization of a Rail Joint[1]
- OS-T: 4010 Size Optimization of a Welded Bracket[1]
- OS-T: 4020 Composite Bike Frame Optimization[1]
- OS-T: 4030 Discrete Size Optimization of a Welded Bracket[1]
- OS-T: 4040 Size Optimization of a Shredder[1]
- OS-T: 4050 Optimization of a Horizontal Tail Plane[1]
- OS-T: 4070 Free-sizing Nonlinear Gap Optimization on an Airplane Wing Rib[1]
- OS-T: 4080 Minimization of the Maximum Stress of a Rotating Bar: A Size Optimization[1]
- OS-T: 4090 Manufacturing Constraints in a Free-size Optimization of a Composite Structure[1]
- OS-T: 4095 Size Optimization using External Responses (DRESP3)[1]
- OS-T: 5000 2D Shape Optimization of a Cantilever Beam[1]
- OS-T: 5010 Cantilever L-beam Shape Optimization[1]
- OS-T: 5020 3D Bracket Model using the Free-shape Method[1]
- OS-T: 5030 Buckling Optimization of a Structural Rail[1]
- OS-T: 5040 Rail Joint[1]
- OS-T: 5050 4 Bar Linkage[1]
- OS-T: 5060 3D Model using the Free-shape Method with Manufacturing Constraints[1]
- OS-T: 5070 Fatigue Optimization of a Torque Control Arm[1]
- OS-T: 5080 Global Search Optimization[1]
- OS-T: 5090 Thermal Optimization on Aluminum Fins[1]
- OS-T: 5100 Stress Response based on Neuber Correction Method[1]
- OS-T: 6010 Multiaxial Fatigue Analysis (Damage Calculation) using S-N Approach[1]
- OS-T: 6020 Multiaxial Fatigue Analysis (strain - life ) using E-N Approach[1]
- OS-T: 6030 seam weld fatigue[1]
- OS-T: 6040 Spot Weld Fatigue[1]
- OS-T: 6050 Dang Van Criterion (Factor of Safety[1]
- OS-T: 6060 Random Response Fatigue Analysis[1]
- OS-T: 6070 Random Response Fatigue Analysis (EN Fatigue[1]
- OS-T: 6080 Sine Sweep Fatigue Analysis (SN Damage)[1]
- OS-T: 6090 Sine Sweep Fatigue Analysis (EN Damage)[1]
- OS-T: 7000 phone drop test analysis[1]
- OS-V: 0270 torsional creep of circular shaft[1]
- OS-V: 0280 Axisymmetric Elements - Interference Fit Between Two Cylinders[1]
- OS-V: 0290 Lee's Frame Postbuckling[1]
- OS-V: 0900 Constant Amplitude Stress-Life Analysis[1]
- OS-V: 1000 Complex Eigenvalue Analysis of Rotor Bearing[1]
- OS-V: 1010 Complex Eigenvalue Analysis of Rotor Bearing[1]
- OS-V: 1100 transmission loss in a muffler[1]
- OS-V: 1200 Bar Impact[1]
- other factors affecting fatigue[1]
- other output controllers - defaults[1]
- OTIME -[1]
- OUTFILE -[1]
- output[1]
- output2 file (.op2[1]
- OUTPUT -[1]
- output - cohesive zone modeling[1]
- output data[1]
- output files - general run and troubleshooting info[1]
- output files generated by the optimization process[1]
- output format controls[1]
- output from contact analysis[1]
- output - linear transient analysis by fourier transformation[1]
- output - modal frequency response analysis[1]
- output - normal modes analysis[1]
- output request - ACCELERATION[1]
- output request - acoustic intensity[1]
- output request - CSTRESS[1]
- output request - DISPLACEMENT[1]
- output requests and ESLM[1]
- output request - STRAIN[1]
- output request - VELOCITY[1]
- overlap - seam weld fatigue analysis[1]
- overview[1]
- P
- P2G - subcase information entry[1]
- P2GSUB - subcase information entry[1]
- PAABSF -[1]
- PACABS -[1]
- PACINF -[1]
- PANEL -[1]
- PANELG -[1]
- PARAM -[1]
- PARAM, ACMODL12-[1]
- PARAM, AGGPCH -[1]
- PARAM, AKUSMOD -[1]
- PARAM, ALLFT -[1]
- PARAM, ALPHA1 -[1]
- PARAM, ALPHA1FL -[1]
- PARAM, ALPHA2 -[1]
- PARAM, ALPHA2FL -[1]
- PARAM, AMLS -[1]
- PARAM, AMLSASPC -[1]
- PARAM, AMLSMAXR -[1]
- PARAM, AMLSMEM -[1]
- PARAM, AMLSNCPU -[1]
- PARAM, AMLSUCON -[1]
- PARAM, AMSE4CMS -[1]
- PARAM, AMSE4EFM -[1]
- PARAM, AMSESLM -[1]
- PARAM, ASCOUP -[1]
- PARAM, AUTOMSET -[1]
- PARAM, AUTOSPC -[1]
- PARAM, AUTOSPRT -[1]
- param, beamalt -[1]
- PARAM, BUFFSIZE -[1]
- PARAM, BUSHRLMT -[1]
- PARAM, BUSHSTIF -[1]
- PARAM, BUSHTLMT -[1]
- PARAM, CB2 -[1]
- PARAM, CDITER -[1]
- PARAM, CDPCH -[1]
- PARAM, CDPRT -[1]
- PARAM, CHECKEL -[1]
- PARAM, CHECKMAT -[1]
- PARAM, CHKELSET -[1]
- PARAM, CHKGPDIR-[1]
- PARAM, CK2 -[1]
- PARAM, CK3 -[1]
- PARAM, CM2 -[1]
- PARAM, CMFTINIT -[1]
- PARAM, CMFTSTEP -[1]
- PARAM, CMSALOAD -[1]
- PARAM, CMSDIRM -[1]
- PARAM, CMSOFST -[1]
- PARAM, CNST4FAT -[1]
- PARAM, COEFFC -[1]
- PARAM, COMP2SHL -[1]
- PARAM, COMPSHST -[1]
- PARAM, CONTFEL -[1]
- PARAM, COUPMASS -[1]
- PARAM, CP2 -[1]
- PARAM, CRTELEM -[1]
- PARAM, CSTEVAL -[1]
- PARAM, CSTOL -[1]
- PARAM, CTSTF4PL -[1]
- PARAM, CURVSHL2 -[1]
- PARAM, DDMNGRPS -[1]
- PARAM, DFREQ -[1]
- PARAM, DISIFMCK -[1]
- PARAM, DISJOINT -[1]
- PARAM, DISPFIC -[1]
- PARAM, DSZERO -[1]
- PARAM, DUPTOL -[1]
- PARAM, EDGESTR -[1]
- PARAM, EFFMAS -[1]
- PARAM, EHD -[1]
- PARAM, ELASRLMT -[1]
- PARAM, ELASSTIF -[1]
- PARAM, ELASTLMT -[1]
- PARAM, ENFMOTN -[1]
- PARAM, EPZERO -[1]
- PARAM, ERPAREA -[1]
- PARAM, ERPC -[1]
- PARAM, ERPREFDB -[1]
- PARAM, ERPRHO -[1]
- PARAM, ERPRLF -[1]
- PARAM, EXCEXB -[1]
- PARAM, EXCOP2 -[1]
- PARAM, EXCOUT -[1]
- PARAM, EXPERTNL -[1]
- PARAM, EXPISOP -[1]
- PARAM, EXTOUT -[1]
- PARAM, FASTCONT -[1]
- PARAM, FASTFR -[1]
- PARAM, FFRS -[1]
- PARAM, FFRSLFREQ -[1]
- PARAM, FFRSMEM -[1]
- PARAM, FFRSNCPU -[1]
- PARAM, FIXRBE3 -[1]
- PARAM, FLEXH3D -[1]
- PARAM, FLIPOK -[1]
- PARAM, FLLWER -[1]
- PARAM, FRIC -[1]
- PARAM, FZERO -[1]
- PARAM, G -[1]
- PARAM, GAPOFFST -[1]
- PARAM, GE4FRSTF -[1]
- PARAM, GE4TRSTF -[1]
- PARAM, GE_MOD -[1]
- PARAM, GFL -[1]
- PARAM, GLOBEXPT -[1]
- PARAM, GMAR1 -[1]
- PARAM, GMAR -[1]
- PARAM, GPSLOC -[1]
- PARAM, GRDPNT -[1]
- PARAM, GRDPNTCM -[1]
- PARAM, GRIDFORM -[1]
- PARAM, GYRO1D -[1]
- PARAM, GYROAVG -[1]
- PARAM, GYROTIMO -[1]
- PARAM, HASHASSM -[1]
- PARAM, HFREQ -[1]
- PARAM, HFREQFL -[1]
- PARAM, HGHCMPOK -[1]
- PARAM, HOURGLS -[1]
- PARAM, I64SLV -[1]
- param, implout -[1]
- PARAM, INREL -[1]
- PARAM, INRGAP -[1]
- PARAM, INTRFACE -[1]
- PARAM, IR4NLCON -[1]
- PARAM, ISTRSBAL -[1]
- PARAM, ITAPE -[1]
- PARAM, K4CUTOFF -[1]
- PARAM, K4METH -[1]
- PARAM, KDAMP -[1]
- PARAM, KGRGD -[1]
- PARAM, KISSSOFT -[1]
- PARAM, KTPLAST -[1]
- PARAM, LFREQ -[1]
- PARAM, LFREQFL -[1]
- PARAM, LGDISP -[1]
- PARAM, LMSOUT -[1]
- PARAM, LOWRANK -[1]
- PARAM, LSNLEXP -[1]
- PARAM, MASSDMIG -[1]
- PARAM, MAXDAMP -[1]
- PARAM, MAXRATIO -[1]
- PARAM, MBDH3D -[1]
- PARAM, MBDREC -[1]
- PARAM, MDK4OPT -[1]
- PARAM, MEMTRIM -[1]
- PARAM, MFILTER -[1]
- PARAM, MODETRAK -[1]
- PARAM, MVASPCON -[1]
- PARAM, NBZRCSR -[1]
- PARAM, NEGMASS -[1]
- PARAM, NEWCRD -[1]
- PARAM, NLAFILE -[1]
- PARAM, NLFAT -[1]
- PARAM, NLINISOL -[1]
- PARAM, NLMON -[1]
- PARAM, NLRFILE -[1]
- PARAM, NLRUN -[1]
- PARAM, NOUTCYC -[1]
- PARAM, NPRBAR -[1]
- PARAM, NPRBE2 -[1]
- PARAM, NPRGDE -[1]
- PARAM, NUMEG -[1]
- PARAM, ODS -[1]
- PARAM, OGEOM -[1]
- PARAM, OMACHPR -[1]
- PARAM, OMID -[1]
- PARAM, OP2GM34 -[1]
- PARAM, ORIGK4[1]
- PARAM, OSTTSPRT -[1]
- PARAM, PBTFCAP[1]
- PARAM, PBUSHT -[1]
- PARAM, PBUSHTF -[1]
- param, peactdmg -[1]
- PARAM, PELAST -[1]
- PARAM, PLIGEXT -[1]
- PARAM, PNLSIZ -[1]
- PARAM, POST -[1]
- PARAM, POSTEXT -[1]
- PARAM, PRESUBNL -[1]
- PARAM, PRGPST -[1]
- PARAM, PRINFACC -[1]
- PARAM, PRTDES -[1]
- PARAM, PRTMGG -[1]
- PARAM, PRTNORM -[1]
- PARAM, PRTRENUM -[1]
- PARAM, PRTRET -[1]
- PARAM, PSDPRINC -[1]
- PARAM, RBE2FREE -[1]
- PARAM, RBE3COL -[1]
- PARAM, RBE3FREE -[1]
- PARAM, RBMEIG -[1]
- PARAM, REANAL -[1]
- PARAM, RECOVER -[1]
- PARAM, REFPNT -[1]
- PARAM, RENUMOK -[1]
- PARAM, RFIOUT -[1]
- PARAM, RHOCP -[1]
- PARAM, RICARDO -[1]
- PARAM, ROMAX -[1]
- PARAM, RSPLICOR -[1]
- PARAM, S2K -[1]
- PARAM, SBTOLRTR -[1]
- PARAM, SEP1XOVR -[1]
- PARAM, SEPLOT -[1]
- PARAM, SH4NRP -[1]
- PARAM, SHELLTI -[1]
- PARAM, SHELOS11 -[1]
- PARAM, SHL2MEM -[1]
- PARAM, SHPBCKOR -[1]
- PARAM, SIGMA -[1]
- PARAM, SIMPACK -[1]
- PARAM, SIMVER -[1]
- PARAM, SMDISP -[1]
- PARAM, SNAPTHRU -[1]
- PARAM, SORTCON -[1]
- PARAM, SPLC -[1]
- PARAM, SPLFAC -[1]
- PARAM, SPLREFDB -[1]
- PARAM, SPLRHO -[1]
- PARAM, SRCOMPS -[1]
- PARAM, SS2GCR -[1]
- PARAM, STRTHR -[1]
- PARAM, TABS -[1]
- PARAM, TCLTINIT -[1]
- PARAM, TCLTSTEP -[1]
- PARAM, THCNTPEN -[1]
- PARAM, THMLSTN -[1]
- PARAM, TOLRSC -[1]
- PARAM, TPS -[1]
- PARAM, TRAKMETH -[1]
- PARAM, TRAKMTX -[1]
- PARAM, UCORD -[1]
- PARAM, UHT -[1]
- param, unsm2sm -[1]
- PARAM, UNSYMSLV -[1]
- PARAM, VMMASS -[1]
- PARAM, VMOPT -[1]
- PARAM, W3 -[1]
- PARAM, W4 -[1]
- PARAM, WR3 -[1]
- PARAM, WR4 -[1]
- PARAM, WRH -[1]
- PARAM, WTMASS -[1]
- PARAM, XPOST -[1]
- parameters for ESLM - nonlinear response optimization[1]
- parts and instances - connectivity[1]
- parts and instances - parts[1]
- pattern grouping[1]
- pattern grouping - circular[1]
- pattern grouping - cyclical[1]
- pattern grouping - cylindrical[1]
- pattern grouping - linear[1]
- pattern grouping - none[1]
- Pattern Grouping Options[1]
- pattern grouping - planar[1]
- pattern grouping - radial 2D[1]
- pattern grouping - radial 2D and linear[1]
- pattern grouping - radial 3D[1]
- pattern grouping - topology optimization[1]
- pattern grouping - vector defined[1]
- pattern repetition for topography optimization[1]
- pattern repetition for topology optimization[1]
- pattern repetition - free-size[1]
- PAXI -[1]
- PBAR -[1]
- PBARL -[1]
- PBARX -[1]
- PBEAM -[1]
- PBEAML -[1]
- PBEAMX -[1]
- PBUSH1D -[1]
- PBUSH -[1]
- PBUSHFX -[1]
- PBUSHT -[1]
- PCG - solvers[1]
- PCNTX2 -[1]
- PCNTX5 -[1]
- PCNTX7 -[1]
- PCNTX11 -[1]
- PCNTX20 -[1]
- PCNTX24 -[1]
- PCOHE -[1]
- PCOMP -[1]
- PCOMPG -[1]
- PCOMPLS -[1]
- PCOMPP -[1]
- PCOMPX -[1]
- PCONT -[1]
- PCONTHT -[1]
- PCONTX -[1]
- PCONV -[1]
- PCONVLIB -[1]
- PDAMP -[1]
- PEAKOUT -[1]
- PEAKOUT - subcase information entry[1]
- PELAS -[1]
- PELASFX -[1]
- PELAST -[1]
- penalty-based contact[1]
- PERBC -[1]
- performance of speaker model - hi-tech electronic applications[1]
- periodic boundary conditions example[1]
- PFAST -[1]
- PFAT -[1]
- PFATSMW -[1]
- PFATSPW -[1]
- PFBODY -[1]
- PFGRID - I/O Options Entry[1]
- PFMODE -[1]
- PFPANEL -[1]
- PFPATH -[1][2]
- PGAP -[1]
- PGAPHT -[1]
- PGASK -[1]
- phase transitions in the optimization of composite structures[1]
- PHFSHL -[1]
- phone drop simulation - hi-tech electronic applications[1]
- pin-ended double cross (Test No. FV2)[1]
- PJOINTG -[1]
- plate in torsion example - topography optimization[1]
- plate with central hole using NLOUT example[1]
- platforms - OptiStruct[1]
- PLOAD1 -[1]
- PLOAD2 -[1]
- PLOAD4 -[1]
- PLOAD -[1]
- PLOADE1 -[1]
- PLOADSF -[1]
- PLOADX1-[1]
- plot convergence during analysis[1][2][3]
- PLOTEL3 -[1]
- PLOTEL4 -[1]
- PLOTEL -[1]
- PLSOLID -[1]
- PLY -[1]
- ply-based laminate modeling[1]
- PMASS -[1]
- point force[1]
- poroelastic materials[1]
- poroelastic materials supported solution sequences[1]
- porosity control - lattice structure optimization[1]
- Post-process - Features[1]
- post-process transfer path analysis[1]
- POST - subcase information entry[1]
- POWERFLOW -[1]
- powertrain applications[1]
- PPLANE -[1]
- PRBODY -[1]
- preloaded modal frequency response analysis[1]
- preload to linear subcases example[1]
- Pre-process - Features[1]
- PRESSURE -[1]
- prestressed complex eigenvalue analysis[1]
- prestressed linear analysis[1]
- prestressed linear analysis results[1]
- prestressed linear analysis types[1]
- prestressed normal modes analysis[1]
- prestressed static analysis[1]
- PRETBOLT -[1]
- PRETENS -[1]
- pretension analysis of piston[1]
- pretension analysis using gasket material example[1]
- pretensioned bolt analysis[1]
- pretensioned bolt analysis comments[1]
- PRETENSION - subcase information entry[1]
- PRETPRM -[1]
- PRETPRM, INILOAD[1]
- PRETPRM, PRTSW[1]
- previous (OS3.5) input format[1]
- previously supported input[1]
- problem formulation - free-size optimization[1]
- problem setup - nonlinear direct transient analysis[1]
- problem setup - nonlinear explicit analysis[1]
- problem setup - nonlinear static analysis[1]
- PROD -[1]
- PROPERTY -[1]
- PSD and RMS responses[1]
- PSEAM -[1]
- PSEC -[1]
- PSHEAR -[1]
- PSHELL -[1]
- PSHELLX -[1]
- PSLDX6 -[1]
- PSOLID -[1]
- PSOLIDX -[1]
- PSURF -[1]
- PTADD -[1]
- PTADJS1 -[1]
- PTADJST -[1]
- PTFORC1 -[1]
- PTFORCE -[1]
- PTUBE -[1]
- punch file - acceleration[1]
- punch file - displacement[1]
- punch file - force[1]
- punch file - multipoint constraint force[1]
- punch file - stress[1]
- punch file - velocity[1]
- PVISC -[1]
- PWELD -[1]
- Q
- QBDY1 -[1]
- quasi-static analysis - MBD[1]
- QVOL -[1]
- QVOLLIB - Bulk Data Entry[1]
- R
- RADBC -[1]
- radial 2d and linear pattern grouping[1]
- radial (3d) pattern grouping[1]
- radial point load on a hemisphere (LE3) verification problem[1]
- radial stretching of cylinder[1]
- radiated sound output analysis[1]
- radiated sound output analysis - at microphone location[1]
- radiated sound output analysis - source grid location[1]
- radiated sound output analytical background[1]
- Radioss[1][2]
- RADM -[1]
- RADPRM -[1]
- RADPRM, HMMOVE -[1]
- RADPRM, HMNAME -[1]
- RADPRM, NLAFILE -[1]
- RADPRM, NLRFILE -[1]
- RADPRM, NLRUN -[1]
- RADPRM, RBE2RBD -[1]
- RADPRM, SH4NRP -[1]
- RADPRM, SMDISP -[1]
- RADPRM, SNAPTHRU -[1]
- RADPRM, XPENTA15 -[1]
- RADSND -[1]
- RADSND - subcase information entry[1]
- random response analysis[1]
- random response analysis - example results[1]
- random response analysis - internal responses[1][2]
- random response analysis plot output[1]
- random response analysis results output[1]
- random response analysis setup[1]
- random response - defaults[1]
- random response fatigue analysis[1]
- random response fatigue analysis - .rnf file[1]
- random response fatigue analysis input[1]
- random spectrum analysis governing equations[1]
- RANDOM - subcase information entry[1]
- random vibration analysis - hi-tech electronic applications[1]
- RANDPS -[1]
- RANDT1 -[1]
- RBADD -[1]
- RBAR -[1]
- RBE2 -[1]
- RBE2GS -[1]
- RBE3 -[1]
- RBODY -[1][2]
- RCROSS -[1][2]
- Recover MBD Analysis Results[1]
- rectangular composite panel example[1]
- rectangular pressure vessel example - topography optimization[1]
- RecurDyn[1]
- reference plane for quadrilateral element or face[1]
- relaxation at constant twist - verification[1]
- release notes - OptiStruct 2020[1]
- reliability-based design optimization[1]
- reliability-based design optimization - implementation[1]
- reliability-based topology optimization of a plate, example[1]
- RELOC -[1]
- relocation - parts and instances[1]
- RENERGY - subcase information entry[1]
- REPCASE - subcase information entry[1]
- REPGLB - subcase information entry[1]
- REPSUB - subcase information entry[1]
- REQUEST -[1]
- requestg radiated sound output guide[1]
- request linear transient heat transfer analysis[1]
- response spectrum analysis[1]
- response spectrum analysis (RSA) optimization example[1]
- response spectrum analysis example[1]
- response spectrum analysis input specification[1]
- RESPRINT -[1]
- RESTART -[1]
- restart of NLSTAT followed by complex eigenvalue analysis[1]
- RESTARTR -[1]
- RESTARTW -[1]
- result files - transfer path analysis[1]
- RESULTS -[1]
- results of a finite element analysis[1]
- results of multibody dynamic analysis[1]
- results - thermal analysis[1]
- RESVEC - subcase information entry[1]
- revolute joint using JOINTG and MOTNJG[1]
- RFORCE -[1]
- RGYRO -[1]
- RGYRO - subcase information entry[1]
- Ricardo[1]
- RIGID -[1]
- rigid body modes - modeling errors[1]
- rigid body motion weight checking[1]
- rigid elements and multi-point constraints[1]
- RJOINT -[1]
- RLOAD1-[1]
- RLOAD2 -[1]
- RNFLOW -[1]
- ROMAX[1]
- rotating bar example - optimization with ESLM[1]
- rotating shell example - optimization with ESLM[1]
- ROTATION -[1]
- rotor dynamics[1]
- rotor dynamics - direct transient response analysis[1]
- rotor dynamics linear static analysis example[1]
- rotor dynamics modal complex eigenvalue analysis example[1]
- ROTORG -[1][2]
- rotor superelements - rotor dynamics[1]
- rotor unbalance example[1]
- RROD -[1]
- RSPEC -[1]
- RSPEC - subcase information entry[1]
- RSPEED -[1]
- RSPINR -[1]
- RSPINT -[1]
- RSPLINE -[1]
- RSSCON -[1]
- rubber ring: crush and slide using self-contact[1]
- rules for substituion - symbolic substitution[1]
- run controls - default[1]
- run FSI[1]
- run modal frequency response analysis[1]
- running OSSmooth[1]
- run options[1]
- runtime monitoring - nonlinear optimization[1]
- run transfer path analysis[1]
- RVDOF1[1]
- RVDOF -[1]
- RWALADD -[1]
- RWALL -[1]
- RWALL - subcase information entry[1]
- S
- SACCELERATION -[1]
- sandwich shell (Test No: R0031/3)[1]
- save and retrieve normal modes analysis results[1]
- scalability - solvers[1]
- Scordelis-Lo roof verification problem[1]
- SCREEN -[1]
- SDAMPING - subcase information entry[1]
- SDISPLACEMENT -[1]
- SEALL - subcase information entry[1]
- seam weld fatigue analysis[1]
- seam weld fatigue analysis and size optimization of a frame structure[1]
- seam weld fatigue analysis implementation[1]
- seam weld fatigue analysis input/output[1]
- SECSET1 -[1]
- SECSET -[1]
- SECT -[1]
- SECTION -[1]
- SEDR - subcase information entry[1]
- SEINTPNT - subcase information entry[1]
- SENSITIVITY -[1]
- sensitivity analysis - gradient-based optimization[1]
- SENSOR -[1]
- SENSOUT -[1]
- SEQSET1 -[1]
- SEQSET -[1]
- SESET -[1]
- SET1 -[1]
- SET3 -[1]
- SET -[1]
- SET/PSET -[1]
- set analysis parameters to include an external field[1]
- SETREE -[1]
- setup transfer path analysis[1]
- SHAPE -[1]
- shape and size optimization of a plate bending example[1]
- shape optimization[1]
- shape optimization example problems[1]
- Shape Optimization - Features[1]
- shape optimization - introductory example[1]
- shape optimization of an oil pan using ERP response[1]
- shape optimization of a solid control arm example[1]
- shape optimization of a stamped hat section example[1]
- shape optimization of connecting rod with fatigue[1]
- shape optimization on a cylinder block with bore distortion responses[1]
- shape optimization on a cylinder head with fatigue responses[1]
- shape optimization results[1]
- Shape Optimization Tutorials[1]
- shared memory parallelization[1]
- shell bending under tip load[1]
- shell elements[1]
- SHRES -[1]
- side constraints - free-shape optimization[1]
- SIMPACK[1]
- simple beam property[1]
- simple symmetry[1]
- simply supported beam verification problem[1]
- simply-supported solid square plate (Test No. FV52)[1]
- sine sweep fatigue analysis[1]
- sine sweep fatigue analysis - .rnf file[1]
- sine sweep fatigue analysis example[1]
- sine sweep fatigue analysis input[1]
- single host - solver script[1]
- single-scale model - MDS modeling[1]
- single-scale results - MDS modeling[1]
- SINTENS -[1]
- size (parameter) optimization[1]
- size (parameter) optimization (phase 2) - lattice structure optimization[1]
- size (parameter) optimization design variables[1]
- size (parameter) optimization example problems[1]
- size (parameter) optimization - features[1]
- size (parameter) optimization of a cantilever beam using equations example[1]
- size (parameter) optimization of a ten bar truss example[1]
- size optimization - shell cantilever example[1]
- Size Optimization Tutorials[1]
- skew plate normal pressure (LE6)[1]
- SLOAD-[1]
- small displacement nonlinear analysis - convergence considerations[1]
- smoothing and remeshing - lattice structure optimization[1]
- smoothing - Laplacian[1]
- SMP (shared memory parallelization)[1]
- SMP implementation[1]
- snap-fit analysis (CONSLI vs FINITE)[1]
- S-N approach[1]
- S-N approach - multiaxial fatigue analysis[1]
- solid cylinder/taper/sphere - temperature (LE11)[1]
- solid element property[1]
- solid elements[1]
- solution sequence - data selectors[1]
- solution sequences - aerospace[1]
- solve an optimization problem not defined by a finite element model[1]
- solver script on single host[1]
- solver script - Windows machines[1]
- SOLVTYP -[1]
- SOLVTYP - subcase information entry[1]
- source grid location - radiated sound output analysis[1]
- SPC1 -[1]
- SPC -[1]
- SPCADD-[1]
- SPCD -[1]
- SPCFORCE -[1]
- SPC - subcase information entry[1]
- speaker, acoustic performance analysis - hi-tech electronic applications[1]
- speaker, vibro-acoustic performance analysis[1]
- special contact applications[1]
- specialized results outputs[1]
- SPL -[1]
- SPOINT -[1]
- spot weld fatigue analysis[1]
- spot weld fatigue analysis and size optimization of a frame structure[1]
- spotweld fatigue analysis - implementation[1]
- spot weld fatigue - input/output[1]
- SPOWER -[1]
- STACK -[1]
- standard result outputs[1]
- static, eigenvalue, transient and multibody loadcases[1]
- static, transient and multibody loadcases[1]
- static analysis - .rnf file[1]
- static analysis - MBD[1]
- static compliance - subcase dependent[1]
- static condensation[1]
- static loads and boundary conditions[1]
- STATSUB - subcase information entry[1]
- steady-state heat transfer analysis - linear[1]
- steady state thermal analysis with convection loading of a structure with insulator[1]
- stiffness penalization - lattice structure optimization[1]
- straight cantilever beam verification problem[1]
- STRAIN -[1]
- strain-based criteria - cohesive zone modeling[1]
- strain-life approach[1]
- strain-life approach - fatigue analysis[1]
- strain-life approach - mean stress correction[1]
- strain-life sine sweep fatigue analysis[1]
- strains - results of a Finite Element Analysis[1]
- STRENGTH2000 - general output[1]
- STRESS -[1]
- stress and strain responses based on the Neuber correction method[1]
- stress-based criteria - damage model method[1]
- stress constraints - lattice structure optimization[1]
- stresses - results of a finite element analysis[1]
- stress-life approach[1][2]
- stress-life sine sweep fatigue analysis[1]
- stress punch file[1]
- stress punch file - frequency response analysiS[1]
- stress punch file - general (default) or random output (random)[1]
- stress punch file - linear and nonlinear static analysis[1]
- stress punch file - linear transient response analysis[1]
- stress punch file - random response analysis[1]
- stress responses for topology and free-size optimization[1][2]
- structural analysis[1]
- structural fluid-structure interaction analysis[1]
- structural fluid-structure interaction analysis - input/output[1]
- structural FSI - monitor[1]
- Structural Optimization - Features[1]
- subcase dependent - internal responses[1]
- subcase independent - internal responses[1]
- subcase information entries by function[1]
- subcase information section[1]
- subcase specific model change using 3-rings example[1]
- subcase specific modeling[1]
- SUBCASE - subcase information entry[1]
- SUBCOM - subcase information entry[1]
- SUBMODEL - subcase information entry[1]
- SUBSEQ - subcase information entry[1]
- SUBTITLE -[1]
- summary - aerospace[1]
- summary information[1]
- SUPER - subcase information entry[1]
- SUPORT1 -[1]
- SUPORT1 - subcase information entry[1]
- SUPORT -[1]
- SUPORT-based fast contact[1]
- supported platforms[1]
- supported solution sequences[1]
- supported solution sequences - cohesive zone modeling[1]
- supported solution sequences - poroelastic materials[1]
- supported solution sequences - rotor dynamics[1]
- supported weld types[1][2]
- SURF -[1]
- surface optimization of a control arm[1]
- surface reduction and surface smoothing[1]
- surface smoothing[1]
- surface-to-surface discretization[1]
- suspension bridge example[1]
- SVELOCITY -[1]
- SWLDPRM -[1]
- SWLDPRM, CHKRUN -[1]
- SWLDPRM, CNRAGLI -[1]
- SWLDPRM, CNRAGLO -[1]
- SWLDPRM, GMCHK[1]
- SWLDPRM, GSMOVE -[1]
- SWLDPRM, GSPROJ -[1]
- SWLDPRM, GSTOL -[1]
- SWLDPRM, NREDIA -[1]
- SWLDPRM, PATEXT -[1]
- SWLDPRM, PROJTOL -[1]
- SWLDPRM, PRTSW -[1]
- SWLDPRM, SHOWAUX -[1]
- symbolic sybstitution[1]
- symmetry three planes[1]
- symmetry - two planes[1]
- SYSSETTING -[1]
- system identification - design optimization[1]
- T
- TABDMP1 -[1]
- TABFAT -[1]
- TABLED1 -[1]
- TABLED2 -[1]
- TABLED3 -[1]
- TABLED4 -[1]
- TABLEG -[1]
- TABLEM1 -[1]
- TABLEM2 -[1]
- TABLEM3 -[1]
- TABLEM4 -[1]
- TABLEMD -[1]
- TABLES1 -[1]
- TABLEST -[1]
- TABLEXN -[1]
- TABRND1 -[1]
- TCURVE -[1]
- TEMP -[1]
- TEMPD -[1]
- TEMPERATURE - subcase information entry[1]
- TEMPP1 -[1]
- TEMPT -[1]
- theory: direct matrix input for Finite Element Analysis (Superelements)[1]
- THERMAL -[1]
- thermal analysis[1]
- thermal analysis - hi-tech electronic applications[1]
- thermal analysis results[1]
- thermal contact solver[1]
- thermal contact without static analysis[1]
- thermal fluid-structure interaction analysis[1]
- thermal fluid-structure interaction analysis - hi-tech electronic applications[1]
- thermal fluid-structure interaction analysis - input[1]
- thermal fluid-structure interaction analysis - output[1]
- thermal fluid-structure interaction monitoring[1]
- thermal fluid structure interaction - powertrain applications[1]
- thermal structural analysis input data[1]
- THICKNESS -[1]
- thick plate pressure (LE10)[1]
- THIN -[1]
- TIC -[1]
- TICA -[1]
- TIE -[1]
- time dependent convection coefficient[1]
- TITLE -[1]
- TLOAD1 -[1]
- TLOAD2 -[1]
- TMPDIR -[1]
- topography optimization[1]
- topography optimization design variables[1]
- topography optimization example problems[1]
- Topography Optimization - Features[1]
- topography optimization - manufacturability[1]
- topography optimization of heat shields with frequency and/or ERP constraints[1]
- Topography Optimization Tutorials[1]
- topography optimization using pattern grouping - examples[1]
- topology and free-size design characterists[1]
- topology and free-size result interpretation[1]
- topology optimization[1]
- topology optimization - design variables[1]
- topology optimization - draw direction constraints[1]
- topology optimization example problems[1]
- Topology Optimization - Features[1]
- topology optimization - manufacturability[1]
- topology optimization - member size control[1]
- topology optimization of bedplate[1]
- topology optimization of control arm with local stress constraint[1]
- topology optimization of gearbox housings[1]
- topology optimization of V-Bracket using RADOPT[1]
- topology optimization on a cylinder block with bore distortion responses[1]
- Topology Optimization Tutorials[1]
- topology optimization using minimum member size control - example problems[1]
- traction-opening curves method - cohesive zone modeling[1]
- transfer path analysis example[1]
- transfer path analysis - NVH[1]
- transfer path analysis post-processing[1]
- transfer path analysis - result files[1]
- transfer path analysis - setup and run[1]
- transient analysis - hi-tech electronic applications[1]
- transient analysis - MBD[1]
- transient and multibody loadcases[1]
- transient fatigue analysis[1]
- Transient Response Loads and Boundary Conditions[1]
- transient thermal subcase continuation[1]
- TSTEP -[1]
- TSTEPE -[1]
- TSTEPE - subcase information entry[1]
- TSTEPNL-[1]
- TSTEPNL - subcase information entry[1]
- TSTEPNX -[1]
- TSTEP - subcase information entry[1]
- TSTRU - subcase information entry[1]
- TTERM -[1]
- tutorials[1][2]
- tutorials implicit[1][2][3][4]
- tutorials OptiStruct[1]
- twisted cantilever beam verification problem - explicit results[1]
- twisted cantilever beam verification problem - implicit results[1]
- two-dimensional heat transfer with convection (test no. T4)[1]
- two-dimensional Michell-truss[1]
- two-layer stamped control arm example[1]
- two Planes - symmetry[1]
- U
- unbalance frequency - rotor example[1]
- UNBALNC -[1]
- uniaxial fatigue analysis[1]
- UNITS -[1]
- UPDATE -[1]
- update optimization model[1]
- user-defined heat transfer properties[1]
- user-defined material[1]
- user-defined volumetric heat addition[1]
- user responses - internal responses[1]
- USET1 -[1]
- USET -[1]
- V
- validation of finite element model - aerospace[1]
- variable pattern grouping[1]
- variables - symbolic substitution[1]
- vector defined pattern grouping[1]
- VELOCITY -[1]
- velocity punch file[1]
- velocity punch file - frequency response analysis[1]
- velocity punch file - linear transient analysis[1]
- velocity punch file - linear transient analysis by Fourier transformation[1]
- velocity punch file - random response analysis[1]
- verify substituted data fields - symbolic substitution[1]
- vibro-acoustic performance analysis[1]
- virtual fluid mass[1]
- Virtual Lab[1]
- VISCO -[1]
- VISCO - subcase information entry[1]
- volume and thermal compliance responses[1]
- W
- warning message database[1]
- warning messages[1][2][3][4][5][6][7][8][9]
- washing machine simulation - hi-tech electronic applications[1]
- WEIGHTCHECK - subcase information entry[1]
- WEIGHT - subcase information entry[1]
- wrapped thick cylinder[1]
- write external functions - optimization responses[1]
- write external functions - user-defined heat transfer properties[1]
- X
- XDAMP -[1]
- XHISADD -[1]
- XHIST -[1]
- XHIST - subcase information entry[1]
- XSHLPRM -[1]
- XSOLPRM -[1]
- XSTEP -[1]
- XSTEP - subcase information entry[1]
- XTITLE -[1]
- XYPEAK -[1]
- XYPLOT -[1]
- XYPUNCH -[1]
- Y
- Z
- Z-section cantilever (test no. LE5)[1]