Formula%20sheet1[1]

Formula%20sheet1[1] - μ=sin-1(1/M(Angle Mach wave sin 2 2...

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Formula sheet R=287 J/kgK, γ=1.4 Thermodynamics
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Normal shock wave
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Flows through Nozzles, Diffusers and Wind Tunnels
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Oblique Shock Waves:
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Unformatted text preview: μ=sin-1 (1/M) (Angle Mach wave) ) sin( 2 , 2 θ β-= n M M \ Expansion Wave Linear Theory Compressible Flow...
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Formula%20sheet1[1] - μ=sin-1(1/M(Angle Mach wave sin 2 2...

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