Command reference help topics
Aerodynamic Trim Variables Constraints dialog box
| Modeling Object | |
|---|---|
| Name | Specifies a descriptive name for this modeling object. |
| Label | Specifies a unique numerical identifier for this modeling object. |
| Properties | |
| Description | Lets you enter a brief description. Click to open a text editor where you can enter a longer description. |
| Mach Number | Specifies the Mach number to use in the static aeroelastic response analysis. |
| Pressure Altitude | Specifies the pressure altitude to use in the static aeroelastic response analysis. |
| Dynamic Pressure | Specifies the dynamic pressure to use in the static aeroelastic response analysis. |
| Calculate Dynamic Pressure from Pressure Altitude and Mach Number | Calculates the dynamic pressure from the pressure altitude and Mach number that you specify using the International Standard Atmosphere (ISA). |
| Trim Analysis Type | Specifies the trim analysis type.StandardUse to account for structural deformation on the loading.RigidUse to ignore the effect of structural deformation on the loading. |
| Standard Variables | |
| Angle of Attack - R2 (ANGLEA) Angle of Sideslip - R3 (SIDES) Roll Rate - R1 (ROLL) Pitch Rate - R2 (PITCH) Yaw Rate - R3 (YAW) Longitudinal - T1 (URDD1) Lateral Acceleration - T2 (URDD2) Vertical Acceleration - T3 (URDD3) Roll Acceleration - R1 (URDD4) Pitch Acceleration - R2 (URDD5) Yaw Acceleration - R3 (URDD6) | Selects the trim variable |
| Magnitude | Appears when you select a standard trim variable.Lets you assign a numerical value to the trim variable. |
| User Variables | |
| Variable 1 through Variable 10 | Lets you create user-defined trim variables.Select an existing trim variable modeling object from the list or click Create Modeling Object to create a new one.Click Edit to edit the selected modeling object.To filter a long list of modeling objects, click More Options to display options for searching and filtering the modeling objects.For more information, see Filter options. |
| Control Surface Variables | |
| Variable 1 through Variable 10 | Lets you create aerodynamic control surface variables.Select an existing aerodynamic control surface variable modeling object from the list or click Create Aerodynamic Control Surface to create a new one.Click Variable to select an aerodynamic control surface variable from the graphics window or from the Simulation Navigator.Click Edit to edit the selected modeling object.To filter a long list of modeling objects, click More Options to display options for searching and filtering the modeling objects.For more information, see Filter options. |
| Magnitude | Appears when you select an aerodynamic control surface variable.Lets you assign a numerical value to the aerodynamic control surface variable. |
Learn more
Static aeroelastic response analysis (SOL 144)
Quick links
Command reference
Pre/Post video examples
Bulk Entry Descriptions
Simcenter 3D tutorials
Browse Simcenter 3D help by product area
Aerodynamic Trim Variables Constraints dialog box, Simcenter 3D 2021.1 Series
© 2020 Siemens
window.mainLanguage="en_US"
window.delivId=""
window.projectId=""
MathJax.Hub.Config({ TeX: { extensions: ["autoload-all.js"] }, tex2jax: { displayMath: [ ] }, "SVG": { scale: 125 } });
Source: https://docs.sw.siemens.com/en-US/doc/289054037/PL20200601120302950.advanced/xid1855195 · retrieved 2026-07-17