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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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- 1 answers
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Find the enthalpy change, internal energy change and entropy change across a shock wave whose upstream air temperature and pressure …
- 49 views
- 1 answers
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Find the reservoir pressure for a nozzle of a supersonic wind tunnel which has an exit-to-throat area ratio of \(4.441\). …
- 40 views
- 1 answers
- 0 votes
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Find the lift and wave drag coefficients for an infinitely thin flat plate at an angle of attack of \(8^{\circ}\) …
- 52 views
- 1 answers
- 0 votes
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An oblique shock wave is generated with a wave angle of \({30^ \circ }\) in a Mach \(4\) flow, at …
- 57 views
- 1 answers
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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 …
- 38 views
- 1 answers
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What are expansion waves ? How does it originates ?
- 130 views
- 1 answers
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What are shock waves ? How does it originates ?
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- 1 answers
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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 …
- 114 views
- 1 answers
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What is a Mach wave ? How does it forms ?
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- 1 answers
- 0 votes
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Find the magnitude of velocity at point \((2,3)\) for a two-dimensional flow field whose stream function is given by \(\psi = 2x^{2}-y^{2}\).
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