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Why is critical Mach number of a sphere higher than a cylinder ?
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How urban air mobility work?
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What is AWACS?
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What are the instruments that are present inside an aircraft’s cockpit?
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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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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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Find the reservoir pressure for a nozzle of a supersonic wind tunnel which has an exit-to-throat area ratio of \(4.441\). …
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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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Calculate lift, wave-drag and pressure coefficients of an infinitely thin flat plate which is in a Mach \(2.5\) freestream flow at an angle of attack of \(5^{^{\circ}}\), using linearized theory.
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Why is critical Mach number of a sphere higher than a cylinder ?
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Find the velocity, pressure and temperature at, \((0.07\,m, 0.07\,m)\).
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Find the pressure coefficient at this point.
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How urban air mobility work?
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