| タイトル | The calculation of downwash behind supersonic wings with an application to triangular plan forms |
| 本文（外部サイト） | http://hdl.handle.net/2060/19930092021 |
| 著者（英） | Sluder, Loma; Heaslet, Max A; Lomax, Harvard |
| 著者所属（英） | National Advisory Committee for Aeronautics. Ames Aeronautical Lab. |
| 発行日 | 1950-01-01 |
| 言語 | eng |
| 内容記述 | A method is developed consistent with the assumptions of small perturbation theory which provides a means of determining the downwash behind a wing in supersonic flow for a known load distribution. The analysis is based upon the use of supersonic doublets which are distributed over the plan form and wake of the wing in a manner determined from the wing loading. The equivalence in subsonic and supersonic flow of the downwash at infinity corresponding to a given load distribution is proved. |
| レポートNO | 93R21311
NACA-TR-957 |
| 権利 | No Copyright |
