| タイトル | Active cooling design for scramjet engines using optimization methods |
| 本文（外部サイト） | http://hdl.handle.net/2060/19880011285 |
| 著者（英） | Lucas, Stephen H.; Martin, Carl J.; Scotti, Stephen J. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1988-03-01 |
| 言語 | eng |
| 内容記述 | A methodology for using optimization in designing metallic cooling jackets for scramjet engines is presented. The optimal design minimizes the required coolant flow rate subject to temperature, mechanical-stress, and thermal-fatigue-life constraints on the cooling-jacket panels, and Mach-number and pressure contraints on the coolant exiting the panel. The analytical basis for the methodology is presented, and results for the optimal design of panels are shown to demonstrate its utility. |
| NASA分類 | STRUCTURAL MECHANICS |
| レポートNO | 88N20669
NAS 1.15:100581
NASA-TM-100581 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/146734 |
