4.5 Consider a 20° half-angle wedge in a supersonic flow at Mach 3 at standard sea level conditions (p₁ = 2116 lb/ft² an

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4.5 Consider a 20° half-angle wedge in a supersonic flow at Mach 3 at standard sea level conditions (p₁ = 2116 lb/ft² an

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4 5 Consider A 20 Half Angle Wedge In A Supersonic Flow At Mach 3 At Standard Sea Level Conditions P 2116 Lb Ft An 1
4 5 Consider A 20 Half Angle Wedge In A Supersonic Flow At Mach 3 At Standard Sea Level Conditions P 2116 Lb Ft An 1 (147.94 KiB) Viewed 32 times
4.5 Consider a 20° half-angle wedge in a supersonic flow at Mach 3 at standard sea level conditions (p₁ = 2116 lb/ft² and T₁ = 519°R). Calculate the wave angle, the surface pressure, temperature, and Mach number.
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