Abstract
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.
| Original language | English |
|---|---|
| Pages (from-to) | 527-529 |
| Number of pages | 3 |
| Journal | Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics |
| Volume | 26 |
| Issue number | 5 |
| State | Published - Oct 2000 |
| Externally published | Yes |
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