| タイトル | Fuel Injector Design Optimization for an Annular Scramjet Geometry |
| 本文（外部サイト） | http://hdl.handle.net/2060/20030014706 |
| 著者（英） | Steffen, Christopher J., Jr. |
| 著者所属（英） | NASA Glenn Research Center |
| 発行日 | 2003-01-01 |
| 言語 | eng |
| 内容記述 | A four-parameter, three-level, central composite experiment design has been used to optimize the configuration of an annular scramjet injector geometry using computational fluid dynamics. The computational fluid dynamic solutions played the role of computer experiments, and response surface methodology was used to capture the simulation results for mixing efficiency and total pressure recovery within the scramjet flowpath. An optimization procedure, based upon the response surface results of mixing efficiency, was used to compare the optimal design configuration against the target efficiency value of 92.5%. The results of three different optimization procedures are presented and all point to the need to look outside the current design space for different injector geometries that can meet or exceed the stated mixing efficiency target. |
| NASA分類 | Fluid Mechanics and Thermodynamics |
| レポートNO | NASA/TM-2003-212094 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/63484 |
