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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 < ½                         (b) F = ½                      (c) F = 1                          (d) F > 1

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