Question Tag: Compressible flow
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Velocity potential of a subsonic compressible flow is \[\phi(x,y) = V_{\infty}x + \frac{5}{\sqrt{1 – M_{\infty}^{2}}}e^{-2\pi\sqrt{1-M_{\infty}^{2}}y}sin2\pi x\] Freestream velocity, pressure and …
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An airfoil is in airflow with \(0.52\) free stream Mach number. Local Mach number at a given point is \(0.82\). …
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Calculate the average flow Mach number over AB, assuming that M varies linearly along portion AB inside the expansion wave.The …
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Calculate the maximum deflection angle through which a sonic flow can be expanded via a centered expansion wave.
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