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Simple wing: Reference Points calculated incorrectly #20

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ybeyer opened this issue Jun 16, 2022 · 0 comments

Contributor

ybeyer commented Jun 16, 2022

Some reference points are not where they are supposed to be:

Issues:

Control Point

In function: simpleWingLoadParams:

P_cntrl == [in code] xyt_cntrl_pt_wing
sweep angle not considered

CP Error for large sweep angles

In function: simpleWingLoadParams()

variable name in code: wing.x_cp0_camber_wing
x_cp0 uses sin(phi) but should be tan(phi)

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