Air, at an absolute pressure of (60.0 mathrm{kPa}) and (27^{circ} mathrm{C}), enters a passage at (486 mathrm{~m}
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Air, at an absolute pressure of \(60.0 \mathrm{kPa}\) and \(27^{\circ} \mathrm{C}\), enters a passage at \(486 \mathrm{~m} / \mathrm{s}\), where \(A=0.02 \mathrm{~m}^{2}\). At section (1) downstream, \(p=78.8 \mathrm{kPa}\) absolute. Assuming isentropic flow, calculate the Mach number at section (2). Sketch the flow passage.
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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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