Principles of Flight questions
I'm busily revising for ATPL exams and have got a couple of PoF questions that I cant figure out! I've spent ages looking through the books but to no avail. Can anybody tell me how to work it out.
Question goes:
An aircraft is straight and level at a CL of 0.35 and a 1 degree increase in AoA would increase the CL by 0.079. Following a vertical gust that gives a 2% increase in AoA, what increase in load factor would result.
Thanks very much,
Yours baffled and perplexed!
Valiant