Founder
27th Nov 2006, 19:07
if the CL of an airplane in steady horizontal flight is 0,4. An increase in angle of attack of 1° gives an increase in CL by 0.09.
if the AoA is increased by 5° by a vertical gust, what will the load factor be?
I know its 2,13 but what I dont know is why???
Please help =)
if the AoA is increased by 5° by a vertical gust, what will the load factor be?
I know its 2,13 but what I dont know is why???
Please help =)