| タイトル | 30 degree injectors at hypervelocity conditions |
| 著者（英） | Newfield, Mark E.; Loomis, Mark P.; Bogdanoff, David W.; Tam, Tim C.; Cavolowsky, John A.; Zambrana, Horacio A.; Bittner, Robert D. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 1992-07-01 |
| 言語 | eng |
| 内容記述 | Results are presented of the first high-speed propulsion-related experiments performed in the NASA-Ames 16-Inch Shock Tunnel, designed to simulate combustor inlet conditions at approximately Mach 14. Results demonstrate the capability of the tunnel for high-speed propulsion testing and yield data on the performance of 30-deg flush wall injectors tested in the tunnel. The experimental results are compared with those of a CFD analysis. |
| NASA分類 | FLUID MECHANICS AND HEAT TRANSFER |
| レポートNO | 92A48877
AIAA PAPER 92-3288 |
| 権利 | Copyright |
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