A 12% thick airfoil experiences Cp, min, 1 = -0.75 at Moo1=0.85 at 012°. Using transonic similarity = rule, we wish to c
Posted: Thu May 05, 2022 6:23 pm
A 12% thick airfoil experiences Cp, min, 1 = -0.75 at Moo1=0.85 at 012°. Using transonic similarity = rule, we wish to calculate: (a) M2, (b) 02, and (c) Cp, min,2 for an affinely-related airfoil 2 that is 6% thick compared to airfoil 1 (10 pts each). Cp, min, 1= -0.75 t/c=12% Moo1=0.85 α₁=2° t/c=6% M002 Cp, min, 2 α₂