| タイトル | Compressible laminar boundary layers with suction on swept and tapered wings |
| 著者（英） | Kaups, K.; Cebeci, T. |
| 著者所属（英） | Douglas Aircraft Co., Inc. |
| 発行日 | 1977-07-01 |
| 言語 | eng |
| 内容記述 | 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. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 77A37940 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/437489 |
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