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Path: ACPro/ACProAerodynamics
% Aerodynamic model with sideforce from a rudder.
Adds the ground effect and includes a quadratic term for the sideforce
in the drag polar.
Since version 4 (ACT).
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Form:
[cD,cC,cL] = AeroCoefficientPointMass( aE, bE, h, d )
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Inputs
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aE (1,1) Angle of attack
bE (1,1) Sideslip angle
h (1,1) Altitude
d (.) Data structure
.cCScale (1,1) Sideforce scale
.aE0 (1,1) Zero lift angle
.cD0 (1,1) Zero lift drag
.aL (1,1) Induced drag due to the lift
coefficient
.aC (1,1) Induced drag due to the sideforce
coefficient
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Outputs
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cD (1,1) Drag coefficient
cC (1,1) Side force coefficient
cD (1,1) Lift coefficient
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See also GroundEffect and DragPolar
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ACPro: ACProAerodynamics/DragPolar ACPro: ACProAerodynamics/GroundEffect
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