| タイトル | The simulation of a propulsive jet and force measurement using a magnetically suspended wind tunnel model |
| 本文（外部サイト） | http://hdl.handle.net/2060/19940031348 |
| 著者（英） | Goodyer, M. J.; Garbutt, K. S. |
| 著者所属（英） | Southampton Univ. |
| 発行日 | 1994-05-01 |
| 言語 | eng |
| 内容記述 | Models featuring the simulation of exhaust jets were developed for magnetic levitation in a wind tunnel. The exhaust gas was stored internally producing a discharge of sufficient duration to allow nominal steady state to be reached. The gas was stored in the form of compressed gas or a solid rocket propellant. Testing was performed with the levitated models although deficiencies prevented the detection of jet-induced aerodynamic effects. Difficulties with data reduction led to the development of a new force calibration technique, used in conjunction with an exhaust simulator and also in separate high incidence aerodynamic tests. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 94N35855 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/111302 |
