摘要
The wall temperature and pressure in cooper heat sink chamber were measured under different velocity ratios of hydrogen to oxygen during hot fire tests of the shear-coaxial injector. The characteristic velocity efficiency and temperature distribution of the chamber wall were analyzed, and the heat flux distribution along the axial direction of the chamber and the quantity of heat absorbed by the chamber were calculated; and the proportion of the energy released for the propellant was computed. The method provides useful insight into the engineering applications.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 2619-2624 |
| 页数 | 6 |
| 期刊 | Hangkong Dongli Xuebao/Journal of Aerospace Power |
| 卷 | 25 |
| 期 | 11 |
| 出版状态 | 已出版 - 11月 2010 |
指纹
探究 'Investigation on the heat flux of heat sink chamber' 的科研主题。它们共同构成独一无二的指纹。引用此
- APA
- Author
- BIBTEX
- Harvard
- Standard
- RIS
- Vancouver