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1st September 2004 | 00:47
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mstram
Joined:
Mar 2001
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From:
Toronto, Ont, Canada
Quote:
"B) Can we find an angle of attack at which the airplane will not stall below stalling speed? (If I am correct, the answer is "no". Because if such angle existed, it would exceed 15 degree, right?)"
The answer is yes - if you allow the aircraft to descend. You can fly below the stall speed (as defined above) provided you reduce the angle of attack = reduced lift = descending
Ok ...
But can you actually get a plane to fly below
descending 1g stall speed
while making it descend?
Mike
Quote:
C) What is load factor? and how can it affect the indicated stalling speed?
Load Factor
http://142.26.194.131/aerodynamics1/Lift/Page8.html
http://142.26.194.131/aerodynamics1/Lift/Page10.html
The Stall
http://www.av8n.com/how/htm/vdamp.html#sec-stall-intro
mstram
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