| タイトル | Flow visualization and interpretation of visualization data for deflected thrust V/STOL nozzles |
| 本文（外部サイト） | http://hdl.handle.net/2060/19840006079 |
| 著者（英） | Burstadt, P. L.; Kao, H. C.; Johns, A. L. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1984-01-01 |
| 言語 | eng |
| 内容記述 | Flow visualization studies were made for four deflected thrust nozzle models at subsonic speeds. Based on topological rules and the assumption that observed streaks constitute continuous vector fields, available visualization pictures are interpreted and flow patterns on interior surfaces of the nozzles are synthesized. In particular, three dimensional flow structure and separations are discussed. From the synthesized patterns, the overall features of the flow field in a given nozzle can be approximately perceived. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 84N14147
E-1933
NAS 1.15:83554
NASA-TM-83554 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/160852 |
