FixedWing.L2.16 Lift and Drag Excercise - wrong equation

udacity / fcnd-issue-reports

You can use this repository to file issue reports with the Flying Car Nanodegree content.

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Closed xcarnd closed 5 years ago

xcarnd commented 5 years ago

The equation for calculating the trim angle of attack is not correct (according to what the solution is shown).

The numerator of the original equation contains a - C_L term, which should be - C_L_0 instead.

AndyAtUdacity commented 5 years ago

Fixed!