Optimization > Design sensitivity analysis
Design variables
Design variables are independent quantities that the solver can vary to perform a design sensitivity analysis or to achieve an optimum design. Upper and lower limits define the allowable range of variation. For example, you can create a design variable to modify the shell thickness between 0.001 mm and 10 mm from a starting thickness of 0.15 mm. You can add design variables only to a solution, not a subcase.
You can define four types of design variables: property, composite property, material, and connectivity.
Property
This design variable type lets you choose physical properties, such as the T field (thickness) in a PSHELL, the DIM1 in a PBEAML, and so on. In Nastran, this creates a DESVAR and DVPREL1 combination. The following physical property types are supported:
| Property type | Supported fields |
|---|---|
| PBAR | A, I1, I2, J, NSM, C1, C2, D1, D2, E1, E2, F1, F2, K1, K2, I12 |
| PBARL | DIM1, DIM2, DIM3, DIM4, DIM5, DIM6, NSM |
| PBEAM | A(A), I1(A), I2(A), I12(A), J(A), NSM(A), C1(A), C2(A), D1(A), D2(A), E1(A), E2(A), F1(A), F2(A), A(B), I1(B), I2(B), I12(B), J(B), NSM(B), C1(B), C2(B), D1(B), D2(B), E1(B), E2(B), F1(B), F2(B), CW(A), CW(B), N1(A), N2(A), N1(B), N2(B) |
| PBEAML | DIM1(A), DIM2(A), DIM3(A), DIM4(A),DIM5(A), DIM6(A), NSM(A), DIM1(B), DIM2(B), DIM3(B), DIM4(B), DIM5(B), DIM6(B), NSM(B) |
| PBUSH | K1, K2, K3, K4, K5, K6, B1, B2 ,B3, B4 ,B5, B6, GE1, SA, ST, EA, ET, GE2, GE3, GE4, GE5, GE6 |
| PDAMP | B1 |
| PELAS | K1, GE1, S1 |
| PGAP | U0, F0, KA, KB, KT, MU1, MU2 |
| PMASS | M1 |
| PROD | A, J, C, NSM |
| PSHEAR | T, NSM, F1, F2 |
| PSHELL | T, 12I/T**3, TS/T, NSM, Z1, Z2 |
| PTUBE | OD, T, NSM |
| PVISC | CE1, CR1 |
Composite Property
This design variable type lets you choose composite or laminate physical properties such as the NSM field (nonstructural mass) in a PCOMP. In Nastran, this creates a DESVAR and DVPREL1 combination.
You can specify a type of PCOMP or Laminate. The following property fields are supported:
| Reference Plane to Bottom Surface Distance (Z0)Nonstructural Mass (NSM)Allowable Bonding Material Shear Stress (SB)Reference Temperature (TREF) | Damping Coefficient (GE)Ply Thickness (T)Ply Orientation Angle (THETA) |
|---|
If you select Ply Thickness (T) or Ply Orientation Angle (THETA), you must specify whether the design variable affects a single ply or multiple plies.
For multiple plies, the thickness or the orientation angle of the selected plies (specified by material ID in the Plies list) will vary with the same ratio as the design variable changes. For example, if the design variable change is 2.0, the thickness or the orientation angle is doubled for all the selected plies.
In addition, when you select Ply Thickness (T) or Ply Orientation Angle (THETA), you can select the Include Reference Plane to Bottom Fiber Distance (Z0) check box to make sure that a specific relation DVPREL1 is written out at export for the Z0 field in the PCOMP property. The DVPREL1 card is written out only if Z0 represents the middle or top plane of the composite. If Z0 is 0.0 (equivalent to bottom), the relation is not needed. If Z0 is user-defined, an error message is issued at export. For more information, see Design Optimization with Composite Materials.
Material
This design variable type lets you choose material properties such as the Young's Modulus value in a MAT1 material. In Nastran, this creates a DESVAR and DVMREL1 combination. The following material types and properties are supported:
| Material types | Supported fields |
|---|---|
| MAT1 | E, G, NU, RHO, A, TREF, GE |
| MAT2 | G11, G12, G13, G22, G23, G33, RHO, A1, A2, A3, TREF, GE |
| MAT8 | E1, E2, NU12, G12, G1Z, G2Z, RHO, A1, A2, TREF, XT, XC, YT, YC, S, GE |
| MAT9 | G11, G12, G13, G14, G15, G16, G22, G23, G24, G25, G26, G33, G34, G35, G36, G44, G45, G46, G55 |
Connectivity (fields in the element definition)
This design variable type lets you choose element fields such as the ZOFFS field (Z offset) in a CQUAD4 element. In Nastran, this creates a DESVAR and DVCREL1 combination. Fields on the following element types are supported:
| Connectivity entry | Supported fields |
|---|---|
| CBAR | X1, X2, X3, W1A, W2A, W3A, W1B, W2B, W3B |
| CBEAM | X1, X2, X3, W1A, W2A, W3A, W1B, W2B, W3B |
| CBUSH | X1, X2, X3, S, S1, S2, S3 |
| CDAMP2 | B |
| CELAS2 | K, GE, S |
| CGAP | X1, X2, X3 |
| CMASS2 | M |
| CONM1 | M11, M21, M22, M31, M32, M33, M41, M42, M43, M44, M51, M52, M53, M54, M55, M61, M62, M63, M64, M65, M66 |
| CONM2 | M, X1, X2, X3, I11, I21, I22, I31, I32, I33 |
| CONROD | A, J, C, NSM |
| CQUAD4 | THETA, ZOFFS, T1, T2, T3, T4 |
| CQUAD8 | THETA, ZOFFS, T1, T2, T3, T4 |
| CQUADR | THETA, ZOFFS, T1, T2, T3, T4 |
| CTRIA3 | THETA, ZOFFS, T1, T2, T3 |
| CTRIA6 | THETA, ZOFFS, T1, T2, T3 |
| CTRIAR | THETA, ZOFFS, T1, T2, T3 |
Where do I find it?
SOL 200 Design Optimization
| Application | Pre/Post |
|---|---|
| Prerequisite | A Simulation file as the work part and displayed partSimcenter Nastran as the specified solverStructural as the specified analysis typeSOL 200 Design Optimization as the specified solution type |
| Command Finder | Modeling Objects →Type set to Design Variable - Composite Property, Design Variable - Connectivity, Design Variable - Material, or Design Variable - Property |
| Location in dialog box | Solution dialog box→Bulk Data tab→Create Design Variables (next to Design Variables) |
SOL 200 Design Sensitivity Analysis
| Application | Pre/Post |
|---|---|
| Prerequisites | A Simulation file as the work part and displayed partSimcenter Nastran or MSC Nastran as the specified solverStructural or Vibro-Acoustic as the specified analysis typeSOL 200 Design Sensitivity Analysis as the specified solution type |
| Command Finder | Modeling Objects →Type set to Design Variable - Composite Property, Design Variable - Connectivity, Design Variable - Material, or Design Variable - Property |
Design variables, Simcenter 3D 2021.1 Series
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Source: https://docs.sw.siemens.com/en-US/doc/289054037/PL20200601120302950.advanced/id975431 · retrieved 2026-07-17