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Workflow for Aero Lookup Tables

    • March 16, 2026 at 12:56 pm
      sas2400038
      Subscriber

      Hi, I am looking for the best workflow to generate an aerodynamic lookup table for a rocket at mach<0.3

      I need to extract the Drag Coeficient,Lift Coeficient,Pitching moment Coeff, and rRoll damping across a range of Mach numbers and Angles of Attack.

      1. Automation: How do I use the Parameter Set in Workbench to automate these sweeps efficiently?

      2. Roll Damping: Is a Steady-State MRF (Moving Reference Frame) approach sufficient for extracting damping derivatives at these speeds?

      3. Resources: Are there specific Ansys Innovation Courses or tutorials that cover Aerodynamic Derivative extraction?

      Thanks for any guidance

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