9.19 Because of the velocity deficit, U-u, in t the streamlines for flow past a flat plate are not the plate. This deviation can be determine displacement thickness, 8. For air blowing shown in Fig. P9.19, plot the streamline A-BU the edge of the boundary layer (y= 8, at x = is, plot y = y(x) for streamline A-B. Assume layer flow. Streamline A-B U= 1 m/s Edge of boundary layer

Structural Analysis
6th Edition
ISBN:9781337630931
Author:KASSIMALI, Aslam.
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Chapter2: Loads On Structures
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9.19 Because of the velocity deficit, U-u, in the boundary layer,
the streamlines for flow past a flat plate are not exactly parallel to
the plate. This deviation can be determined by use of the
displacement thickness, 8. For air blowing past the flat plate
shown in Fig. P9.19, plot the streamline A-B that passes through
the edge of the boundary layer (y=8, at x = () at point B. That
is, plot y = y(x) for streamline A-B. Assume laminar boundary
layer flow.
Streamline A-B
1 m/s
-Edge of boundary layer
Transcribed Image Text:9.19 Because of the velocity deficit, U-u, in the boundary layer, the streamlines for flow past a flat plate are not exactly parallel to the plate. This deviation can be determined by use of the displacement thickness, 8. For air blowing past the flat plate shown in Fig. P9.19, plot the streamline A-B that passes through the edge of the boundary layer (y=8, at x = () at point B. That is, plot y = y(x) for streamline A-B. Assume laminar boundary layer flow. Streamline A-B 1 m/s -Edge of boundary layer
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