Consider a Mach 2.8 supersonic flow over a compression corner with a deflection angle of (15^{circ}). If

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Consider a Mach 2.8 supersonic flow over a compression corner with a deflection angle of $15^{\circ}$. If the deflection angle is doubled to $30^{\circ}$, what is the increase in shock strength? Is it also doubled?

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Modern Compressible Flow With Historical

ISBN: 9781260570823

4th Edition

Authors: John Anderson

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Question Posted: Apr 16, 2024 07:00 AM

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Consider a Mach 2.8 supersonic flow over a compression corner with a deflection angle of (15^{circ}). If

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From the thetabetaM chart for theta15circ beta338circ and for theta30circ beta547circ For t...View the full answer

Modern Compressible Flow With Historical

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