| タイトル | Aerodynamic characteristics of a six-jet V/STOL configuration with four swing-out lift jets in the transition speed range |
| 本文（外部サイト） | http://hdl.handle.net/2060/19720010357 |
| 著者（英） | Carter, A. W. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1970-11-01 |
| 言語 | eng |
| 内容記述 | A wind-tunnel investigation has been made of the longitudinal aerodynamic characteristics and jet-interference effects of a model of a jet V/STOL variable-sweep fighter airplane that employs four direct-lift engines which swing out from the fuselage and two lift-cruise engines located in the rear part of the fuselage. Data were obtained with two wing areas for various forward speeds and power conditions in the transition speed range. The data are presented without analysis or discussion. |
| NASA分類 | AIRCRAFT |
| レポートNO | 72N18007
NASA-TM-X-2060
L-7246 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/204097 |
