| タイトル | Effects of ground proximity on the aerodynamic characteristics of a six-jet V/STOL configuration with four swing-out lift jets |
| 本文（外部サイト） | http://hdl.handle.net/2060/19720010358 |
| 著者（英） | Carter, A. W. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1971-05-01 |
| 言語 | eng |
| 内容記述 | A wind-tunnel investigation has been made of the effects of ground proximity on the longitudinal and lateral-directional 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 ahead of the wing and two lift-cruise engines located in the rear part of the fuselage. Data were obtained through a range of angles of attack and sideslip at simulated speeds from hover through transition at various heights of the model above a moving-belt ground plane. Power-off data and power-on data at several power conditions are presented. The data are presented without analysis or discussion. |
| NASA分類 | AIRCRAFT |
| レポートNO | 72N18008
NASA-TM-X-2212
L-7555 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/204096 |
