Convert lift, drag and side into body axis?

bomber
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Joined: Mon Nov 30, 2015 3:40 pm

Convert lift, drag and side into body axis?

Postby bomber » Tue Oct 25, 2016 5:46 pm

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.
"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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