Question Cagtegory: Aerodynamics
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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 …
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Find the speed of sound in air at a temperature of 250 K.
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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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Why induced drag is minimum for an elliptical wing planform?
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Induced drag is minimum for which type of a wing planform
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With the angle of attacck alpha of 5° and h/c = 0.06
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What is a induced drag ?
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