Review on Transpiration Cooling for Near-Space Aircraft

被引：0
|
作者：
Luan Y. [1 ]
He F. [1 ]
Wang J.-H. [1 ]
机构：
[1] Department of Thermal Science and Energy Engineering, University of Science and Technology of China, Hefei
来源：
Tuijin Jishu/Journal of Propulsion Technology | 2023年 / 44卷 / 01期
关键词：
Active cooling; Combined cooling technology; Near-space aircraft; Review; Structure optimization; Transpiration cooling;
D O I：
10.13675/j.cnki.tjjs.22010020
中图分类号：
学科分类号：
摘要：
Transpiration cooling is an active thermal protection technology for near-space aircraft, which has an extremely high cooling efficiency. Based on a large number of relevant literatures, this paper introduces the mechanism and cooling characteristics of transpiration cooling, and summarizes its research progress in recent years. It mainly includes the selection of matrix material and coolant, the development of investigation method and structural optimization design. Finally, considering the existing problems of transpiration cooling, the possible research directions in the future are proposed. © 2023 Journal of Propulsion Technology. All rights reserved.
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