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Welcome to the FLOWUnsteady wiki!

TODO:

• Integrate FLOWPanel (3D panel code) into FLOWUnsteady

  • Prototype integration
  • Validation cases
    • Duct
    • Swept-back wing
  • Figure out correct way of calculating forces in FLOWPanel at surface
  • Using FLOWPanel as a lifting surface plate (VLM with chord-wise elements)
  • Add OpenVSP geometry import sections relevant to FLOWPanel (after FLOWPanel integration)

• OpenVSP -> FLOWUnsteady coupling

  • OpenVSP integration using VSPGeom package for:
    • wings
    • fuselage
    • props
    • ducts (although same as fuselage component, might have to be handled differently)

• Develop unstructured capabilities of FLOWPanel

• Test non-linear cl capabilities of wing model using the lookup tables

• Shed separated wake from lookup table