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An airplane is flying at an velocity of 100\,m/s. Find the pressure coefficient at a point on the surface of …
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A pitot tube of an airplane which is flying at an standard sea level measures a pressure of \(1.09 \times …
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Find the velocity of an airplane flying at a standard sea level, if the static pressure at the throat of …
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The reservoir of a supersonic wind-tunnel has a total temperature and total pressure of 600\,K and 11\,atm. If the flow …
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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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