| タイトル | Aerodynamic design modification of a hypersonic wind tunnel nozzle by CSCM with high order accuracy |
| 著者（英） | Nagaraj, N.; Lombard, C. K.; Luh, R. C.-C.; Codding, W. H.; Yang, J. Y. |
| 著者所属（英） | PEDA Corp. |
| 発行日 | 1987-06-01 |
| 言語 | eng |
| 内容記述 | An improved version of the CSCM implicit Navier-Stokes solver with a flexible data structure has been applied, in conjunction with a sophisticated patched grid system, to the aerodynamic analysis of hypersonic axisymmetric contoured nozzles of the NASA-Ames 3.5-foot hypersonic wind tunnel. The results obtained are found to be in good agreement with experiment. Based on the analysis, a newly designed throat contour for the Mach 14 nozzle has been recommended. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 87A45284
AIAA PAPER 87-1896 |
| 権利 | Copyright |
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