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Compressible laminar boundary layers with suction on swept and tapered wings (1977)

Kaups, K. ; Cebeci, T.

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Publication Date: 2019-06-27

Description: In this paper we present a numerical method for solving the compressible laminar boundary-layer equations with suction on swept and tapered wings. The method employs an efficient two-point finite-difference method to solve the governing equations, and a very convenient similarity transformation which removes the wall normal velocity as a boundary condition and places it into the governing equations as a parameter. In this way the awkward nonlinear boundary condition which couples all the variables is avoided. To test and demonstrate the method, we present a sample calculation for a typical laminar-flow-control (LFC) wing.

Keywords: AERODYNAMICS

Type: Journal of Aircraft; 14; July 197

Format: text

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