Answered: 5) A wedge airfoil is placed in a…

5) A wedge airfoil is placed in a supersonic flow at M 2. G. Calculate the lift and drag coefficients at 4 angle of attack, Hint: Consider the free-stream pressure at the base of the airfoil, 4° Po

Principles of Heat Transfer (Activate Learning with these NEW titles from Engineering!)

8th Edition

ISBN:9781305387102

Author:Kreith, Frank; Manglik, Raj M.

Publisher:Kreith, Frank; Manglik, Raj M.

Chapter5: Analysis Of Convection Heat Transfer

Section: Chapter Questions

Problem 5.68P

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G is 2.
Hello i need help related with this question.

5) A wedge airfoil is placed in a supersonic flow at M 2, G, Calculate the lift and drag coefficients
at 4 angle of attack,
Hint: Consider the free-stream pressure at the base of the airfoil,
4°-
Poo
24

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