Aerospace Engineering > GATE 2021 > Boundary Layer
Consider a model of a boundary layer with the following velocity profile:
The shape factor, defined as the ratio of the displacement thickness to the momentum thickness, for this profile is _______. (round off to 2 decimal places)

Correct : 4.8 to 5.2

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Related Topics

boundary layer model displacement thickness momentum thickness shape factor GATE Aerospace Engineering 2021 aerodynamics boundary layer equations GATE 2021 fluid dynamics

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