摘要
The flow and heat transfer numerical model for Canopy Thermal Fatigue Test-Bed is established. The simulating results agree with the experiment data well. Based on plenty of calculation results, a new scheme for the induce channel is presented. The application of the new shell makes the temperature difference between the top points in the front and the back of the Canopy within the request range.
源语言 | 英语 |
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页(从-至) | 386-389 |
页数 | 4 |
期刊 | Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica |
卷 | 27 |
期 | 3 |
出版状态 | 已出版 - 5月 2006 |