| タイトル | A comparison of experimental data with CFD for the NSWC Hypervelocity Wind Tunnel No. 9 Mach 14 Nozzle |
| 著者（英） | Hedlund, Eric; Korte, John J.; Anandakrishnan, Satayan |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1992-07-01 |
| 言語 | eng |
| 内容記述 | An experimental and numerical study has been performed of the flow physics occurring in the Naval Surface Warfare Center Hypervelocity Wind Tunnel No.9 Mach 14 Nozzle. Mach 8, 10, 14, and 18 test section conditions are obtained utilizing various axisymmetric contoured wind tunnel nozzles. Numerical and experimental results are presented for the Mach 14 configuration. |
| NASA分類 | RESEARCH AND SUPPORT FACILITIES (AIR) |
| レポートNO | 92A56833
AIAA PAPER 92-4010 |
| 権利 | Copyright |
