chrissak1216 chrissak1216
  • 18-01-2024
  • Engineering
contestada

Given a 2-D airfoil with a 10-degree angle of attack, what parameters need to be determined at lower surfaces, L1 and L2?
a) Mach numbers, lift forces, and drag coefficients
b) Mach numbers, pressure distribution, and flow angles
c) Reynolds numbers, lift forces, and pressure coefficients
d) Flow velocities, drag forces, and lift distribution

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