摘要
The method for installation performance computation of missile turbojet engine was given. Based on the total pressure recovery computation and drag of S inlet, nozzle/afterbody analysis, the computer programs calculating the installation performance of missile turbojet engine were edited. With this program, the effect of customer's bleeding, horsepower extracting, installation of inlet/nozzle and temperature on engine performance were computed. The results indicate that the installation performance should be computed to determine the effect of every installation factors.
| 源语言 | 英语 |
|---|---|
| 页（从-至） | 12-16 |
| 页数 | 5 |
| 期刊 | Tuijin Jishu/Journal of Propulsion Technology |
| 卷 | 24 |
| 期 | 1 |
| 出版状态 | 已出版 - 2月 2003 |