摘要
As the need of thermal-vibration composite test for the high-speed vehicle, a thermal-vibration experimental simulation system was established. This experiment system included the vibration experiment system and the thermal experiment system. In the test process, the thermal experiment system simulated the heating process of high-speed cruise by the air, at the same time the vibration experiment system provided the flight vibration environment to the high-speed cruise. The results of the experiment show that this composite environment experiment system can provide a reliable basis for the safety flight of cruise missile under high-speed, high-temperature and vibration conditions.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 1507-1511 |
| 页数 | 5 |
| 期刊 | Hangkong Dongli Xuebao/Journal of Aerospace Power |
| 卷 | 24 |
| 期 | 7 |
| 出版状态 | 已出版 - 7月 2009 |
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