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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 …
- 550 views
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Find the enthalpy change, internal energy change and entropy change across a shock wave whose upstream air temperature and pressure …
- 629 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 \(4.441\). …
- 462 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 \(8^{\circ}\) …
- 517 views
- 1 answers
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An oblique shock wave is generated with a wave angle of \({30^ \circ }\) in a Mach \(4\) flow, at …
- 616 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 …
- 427 views
- 1 answers
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What are expansion waves? How does it originates?
- 914 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 …
- 863 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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A fluid flowing along a pipe line undergoes a throttling process from 10 bar to 1 bar is passing through a partially open valve. Before throttling, the specific volume of the fluid is 0.5 m^3/kg and after throttling is 2.0 m^3/kg. What is the change in specific internal energy during the throttling process?
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