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Consider a non-lifting flow over a circular cylinder and derive an expression for the pressure coefficient at any arbitrary point …
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Calculate locations on the surface of a cylinder where surface pressure equals to free-stream pressure considering a non-lifting flow.
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Lift per unit span of a spinning circular cylinder in a free stream with velocity of 50 m/s is 8 …
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In an inviscid, incompressible flow of air along a streamline, the air density is 0.002377 {\rm{slug/f}}{{\rm{t}}^{\rm{3}}}. At a point on …
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Consider an airfoil in a flow at standard sea level conditions with a freestream velocity of {\rm{70m/s}}. At a given …
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The temperature and pressure at the stagnation point of a high speed missile are {934^ \circ } R and 7.8 atm, …
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