Desired capability or behavior.
Copied from source code in subsystems/aerodynamics/gasp_based/premission_aero.py: add subsystems to compute CLMXFU, CLMXTO, CLMXLD using dynamic aero components with alpha > alpha_stall.
Here CLMXFU is the lift coefficient with flaps up. CLMXTO and CLMXLD are the lift coefficient when taking off and landing respectively.
Is your feature request related to a problem? Please describe.
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Associated Bug Report
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Desired capability or behavior.
Copied from source code in
subsystems/aerodynamics/gasp_based/premission_aero.py: add subsystems to computeCLMXFU,CLMXTO,CLMXLDusing dynamic aero components with alpha > alpha_stall.Here
CLMXFUis the lift coefficient with flaps up.CLMXTOandCLMXLDare the lift coefficient when taking off and landing respectively.Is your feature request related to a problem? Please describe.
No response
Associated Bug Report
No response