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Find the enthalpy change, internal energy change and entropy change across a shock wave whose upstream air temperature and pressure …
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The upstream Mach number, pressure and temperature of a supersonic flow over an expansion corner having deflection angle \theta =25^{^{\circ}} …
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An oblique shock wave is generated at a compression corner having a deflection angle of 20^{^{\circ}}. The oblique shock wave …
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A flow is passing over a {20^ \circ } half-angle wedge having a upstream Mach number, pressure and temperature of …
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An oblique shock wave is generated with a wave angle of {30^ \circ } in a Mach 4 flow, at …
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Find the upstream Mach number if there is an entropy increase across the normal shock wave of 220\,J/\left( {kg.K} \right).
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A flow passes through a normal shock wave has a pressure, temperature and Mach number of 1\,atm,\,295\,K and 2.8 upstream …
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What are shock waves? How does it originates?
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Calculate the wave drag on the wings of an airplane which is flying at a Mach number of 2.1 at …
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