kinex
28th May 2003, 20:14
I am doing my final uni assignment on Determining the "Stick Fixed Neutral Point "on an aircraft
Can anyone tell me how to calculate the distance from the leading edge to centre of pressure and Aerodynamic Centre on the aerofoil or any information that i can look up from the Internet.
(Assuming that L is linear up to 12 AoA and Coef Lift is 0 if AoA = 0)
thanks
Kinex
Can anyone tell me how to calculate the distance from the leading edge to centre of pressure and Aerodynamic Centre on the aerofoil or any information that i can look up from the Internet.
(Assuming that L is linear up to 12 AoA and Coef Lift is 0 if AoA = 0)
thanks
Kinex