| タイトル | Supersonic Coaxial Jet Experiment for CFD Code Validation |
| 本文（外部サイト） | http://hdl.handle.net/2060/20040086859 |
| 著者（英） | Carty, A. A.; Doerner, S. E.; Cutler, A. D.; Drummond, J. P.; Diskin, G. S. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1999-01-01 |
| 言語 | eng |
| 内容記述 | A supersonic coaxial jet facility has been designed to provide experimental data suitable for the validation of CFD codes used to analyze high-speed propulsion flows. The center jet is of a light gas and the coflow jet is of air, and the mixing layer between them is compressible. Various methods have been employed in characterizing the jet flow field, including schlieren visualization, pitot, total temperature and gas sampling probe surveying, and RELIEF velocimetry. A Navier-Stokes code has been used to calculate the nozzle flow field and the results compared to the experiment. |
| NASA分類 | Aircraft Design, Testing and Performance |
| レポートNO | AIAA Paper 99-3588 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/88508 |
