Question: Consider a symmetrical airfoil with 1 m chord in a wind tunnel experiment where free stream velocity is 37 m/s at sea level conditions.
Consider a symmetrical airfoil with 1 m chord in a wind tunnel experiment where free stream velocity is 37 m/s at sea level conditions. Using the flat plate approximation, estimate the viscous drag at zero angle of attack. (Take poo = 1.225 kg/m3 and oo = 1.778 x 10-5 kg/ms)
Step by Step Solution
3.45 Rating (161 Votes )
There are 3 Steps involved in it
SOLUTION To estimate the viscous drag at zero angle of attack using the flat plate approximation we ... View full answer
Get step-by-step solutions from verified subject matter experts
