Browsing Aeronautical Research Council Reports & Memoranda by Author "P. A. Pinsent"

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An approximate integral method for calculating the incompressible laminar boundary layer on an infinite swept wing on which velocity and suction distribution are arbitrary

H. G. Pinsent; P. A. Pinsent (1959)

Summary. The method described in this Report gives an approximate solution for the cross-flow velocity in an incompressible laminar boundary layer on an infinite swept wing. The cross flow is defined as that velocity in ...

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