Drag force on a flat plate - GATE ME '07
Consider an incompressible laminar boundary layer flow over a flat plate of length L, aligned with the direction of an incoming uniform free stream. If F is the ratio of the drag force on the front half of the plate to the drag force on the rear half, then A. F<1/2 B. F=1/2 C. F=1 D. F>1
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#externalflow #boundarylayer #fluidmechanics
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