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GATE Mechanical Engineering (ME) 2018 Shift 2 Solved Paper

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Question : 27

Total: 65

The viscous laminar flow of air over a flat plate results in the formation of a boundary layer. The boundary layer thickness at the end of the plate of length L is δL. When the plate length is increased to twice its original length, the percentage change in laminar boundary layer thickness at the end of the plate (with respect to δL ) is (correct to two decimal places).

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