| タイトル | Analyzing Transonic Flow Over A Wing And Fuselage |
| 著者（英） | Melson, N. Duane; Streett, Craig L. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1993-02-01 |
| 言語 | eng |
| 内容記述 | TAWFIVE computer program calculates transonic flow over transport-type wing and fuselage. Combines multigrid acceleration technique in iterative solution of potential equation with use of integral-form boundary-layer equations to provide software tool computationally efficient, yet accurate enough for use in design. Simplifies solution process by breaking problem into loosely coupled set of modified equations. Inviscid-flow method, using standard inviscid-flow equations, valid in "outer" region away from wing, whereas boundary-layer equations valid in thin region near solid surface of wing. Written in FORTRAN 77. |
| NASA分類 | MECHANICS |
| レポートNO | 93B10092
LAR-14722 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/323710 |
|
