Aerospace Engineering > GATE 2016 > Boundary Layer Theory
For a laminar incompressible flow past a flat plate at zero angle of attack, the variation of skin friction drag coefficient (Cf) with Reynolds number based on the chord length (Rec) can be expressed as
Correct : c
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Air, with a Prandtl number of 0.7, flows over a flat plate at a high Reynolds number. Which of the following statement is TRUE?
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