| タイトル | Propulsion and airframe aerodynamic interactions of supersonic V/STOL configurations. Volume 4: Summary |
| 本文（外部サイト） | http://hdl.handle.net/2060/19880013484 |
| 著者（英） | Wallace, H. W.; Hiley, P. E.; Zilz, D. E. |
| 著者所属（英） | McDonnell Aircraft Co. |
| 発行日 | 1985-09-01 |
| 言語 | eng |
| 内容記述 | A wind tunnel model of a supersonic V/STOL fighter configuration has been tested to measure the aerodynamic interaction effects which can result from geometrically close-coupled propulsion system/airframe components. The approach was to configure the model to represent two different test techniques. One was a conventional test technique composed of two test modes. In the Flow-Through mode, absolute configuration aerodynamics are measured, including inlet/airframe interactions. In the Jet-Effects mode, incremental nozzle/airframe interactions are measured. The other test technique is a propulsion simulator approach, where a sub-scale, externally powered engine is mounted in the model. This allows proper measurement of inlet/airframe and nozzle/airframe interactions simultaneously. This is Volume 4 of 4: Final Report- Summary. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 88N22868
NAS 1.26:177343-VOL-4
NASA-CR-177343-VOL-4 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/146430 |
|
