Stall question from the Belgium exam
Hope this is the right section to post this.
This is a question from the Belgium exam
A possible cause for the auto recovery of an airplane after a stall is
a. The angle of incidence (AOI) of the wing is larger than the AOI of the stabilizer
b. The wing surface is bigger than the wing surface of the stabilizer.
c. The AOI of the wing is smaller than the AOI of the stabilizer.
d. The angle of attack (AOA) of the stabilizer is bigger than the AOA of the wing.
1. is the right answer but why? Is the question anyhow correct and can you generalise this question for every plane?