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Unlocking everything in Rocket League is a requirement for a number of trophies, and the easily attainable platinum in Rocket …
- 7 views
- 0 answers
- 0 votes
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A velocity field is given by \(u=\frac{y}{x^{2}}\) and \(v=\frac{x}{y^{2}}\). Find the circulation around a circular path of radius \(4\,m\). Units …
- 16 views
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A velocity field is given by \(u=\frac{y}{x^{3}+y^{3}}\) and \(v=\frac{-x}{x^{3}+y^{3}}\). Find its vorticity.
- 14 views
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A velocity field is given by \(u=\frac{y}{x^{3}+y}\) and \(v=\frac{-x}{x^{3}+y}\). Find the equation of the streamline which is passing through the …
- 21 views
- 1 answers
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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 …
- 14 views
- 1 answers
- 0 votes
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Find the enthalpy change, internal energy change and entropy change across a shock wave whose upstream air temperature and pressure …
- 30 views
- 1 answers
- 0 votes
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Find the combustion chamber pressure of a rocket engine using hydrogen and oxygen as propellants, whose mass flow in combustion …
- 39 views
- 1 answers
- 0 votes
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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 \(4.441\). …
- 31 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 \(8^{\circ}\) …
- 36 views
- 1 answers
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The upstream Mach number, pressure and temperature of a supersonic flow over an expansion corner having deflection angle \(\theta =25^{^{\circ}}\) …
- 42 views
- 1 answers
- 0 votes
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Find the nozzle's exit temperature and density if its exit pressure is \(1\,atm\).
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Find the enthalpy change, internal energy change and entropy change across a shock wave.
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Find the combustion chamber pressure of a rocket engine.
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Find the reservoir pressure for a nozzle of a supersonic wind tunnel.
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Find the lift and wave drag coefficients for an infinitely thin flat plate.
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