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美国政府科技报告
>Approximate Calculations of the Laminar Boundary Layer with Suction, with Particular Reference to the Suction Requirements for Boundary-Layer Stability on Aerofoils of Different Thickness/Chord Ratios
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Approximate Calculations of the Laminar Boundary Layer with Suction, with Particular Reference to the Suction Requirements for Boundary-Layer Stability on Aerofoils of Different Thickness/Chord Ratios
In an earlier report1 an account was given of an approximate method for calculating the incompressible laminar boundary layer in two dimensions. Application of the method to the various cases for which exact (or nearly exact) solutions were available gave results which were in all cases in very satisfactory agreement with the accepted solutions. The accuracy of the method (essentially a development of one given earlier by Wieghardt2), evidently resulted from satisfying both the momentum and energy integral equations of the boundary layer, together with the first compatibility condition at the surface.
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