| タイトル | Evaluation of a bulk calorimeter and heat balance for determination of supersonic combustor efficiency |
| 本文（外部サイト） | http://hdl.handle.net/2060/19810004547 |
| 著者（英） | Mcclinton, C. R.; Anderson, G. Y. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1980-12-01 |
| 言語 | eng |
| 内容記述 | Results are presented from the shakedown and evaluation test of a bulk calorimeter. The calorimeter is designed to quench the combustion at the exit of a direct-connect, hydrogen fueled, scramjet combustor model, and to provide the measurements necessary to perform an analysis of combustion efficiency. Results indicate that the calorimeter quenches reaction, that reasonable response times are obtained, and that the calculated combustion efficiency is repeatable within + or -3 percent and varies in a regular way with combustor model parameters such as injected fuel equivalence ratio. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 81N13058
NASA-TP-1739
L-13943 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/170626 |
