Aerospace Engineering > GATE 2009 > Boundary Layer Theory
The laminar boundary layer over a large flat plate held parallel to the flow is 7.2 mm thick at a point
0.33 m downstream of the leading edge. If the free stream speed is increased by 50%, then the new
boundary layer thickness at this location will be approximately
0.33 m downstream of the leading edge. If the free stream speed is increased by 50%, then the new
boundary layer thickness at this location will be approximately
Correct : c
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