摘要
The experimental results were reported about the pressure transient responses and temperature transient responses of the bleed system of an aircraft environmental control system when the bleed air flow, pressure and temperature are varied. The results show that the pressure response is quite fast and response time is within 1 second, while the temperature response time is 10-30 seconds.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 527-529 |
| 页数 | 3 |
| 期刊 | Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics |
| 卷 | 26 |
| 期 | 5 |
| 出版状态 | 已出版 - 10月 2000 |
| 已对外发布 | 是 |
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