Consider an air flow over a flat wall with an upstream velocity of (6 mathrm{~m} / mathrm{s}).

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Consider an air flow over a flat wall with an upstream velocity of \(6 \mathrm{~m} / \mathrm{s}\). There is a narrow slit through which air is drawn in at a flow rate of \(0.2 \mathrm{~m}^{3} / \mathrm{s}\) per meter of width. Represent the flow as a combination of a uniform flow and a sink. Determine the location of the stagnation point. Sketch the dividing line between the air that enters the slit and the air that continues downstream.

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Fox And McDonald's Introduction To Fluid Mechanics

ISBN: 9781118912652

9th Edition

Authors: Philip J. Pritchard, John W. Mitchell

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