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Consider a diamond-wedge airfoil such as shown in the figure below, with a half- angle ε = 100. The airfoil is at an ang
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Consider a diamond-wedge airfoil such as shown in the figure below, with a half- angle ε = 100. The airfoil is at an ang
Consider a diamond-wedge airfoil such as shown in the figure below, with a half- angle ε = 100. The airfoil is at an angle of attack a = 150 to a Mach 3 freestream. Calculate the lift and wave-drag coefficients for the airfoil. ... LIFT Oblique shock Expansion wave Oblique shock Airflow Relative Airflow M>1 -DRAG Angle of Attack
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