https://forum.flightgear.org/search.php ... 43510df09e
Calculate the resultant and from this use the cos and sine of the wings incidence to the fuselage body to find the x and z values.
Convert lift, drag and side into body axis?
Convert lift, drag and side into body axis?
"If anyone ever tells you anything about an aeroplane which is so bloody complicated you can't understand it, take it from me - it's all balls" - R J Mitchell
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