Compute the air density in the undisturbed air and at the stagnation point of an aircraft flying
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Compute the air density in the undisturbed air and at the stagnation point of an aircraft flying at \(250 \mathrm{~m} / \mathrm{s}\) in air at \(28 \mathrm{kPa}\) and \(250^{\circ} \mathrm{C}\). What is the percentage increase in density? Can we approximate this as an incompressible flow?
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Related Book For
Fox And McDonald's Introduction To Fluid Mechanics
ISBN: 9781118912652
9th Edition
Authors: Philip J. Pritchard, John W. Mitchell
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