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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 …
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What are jet engine and scramjet engine ?
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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 lift and wave drag coefficients for an infinitely thin flat plate at an angle of attack of \(8^{\circ}\) …
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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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What are expansion waves ? How does it originates ?
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What are shock waves ? How does it originates ?
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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 …
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What is a Mach wave ? How does it forms ?
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An airplane flying at a Mach number of 2.2 makes a Mach wave at the nose. What angle does it …
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Question Tag: Supersonic airplanes
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