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Thermal-hydraulic characteristics of a PCHE with zigzag microchannel for hypersonic precooled aero-engines: an experimental study
Experimental Heat Transfer ( IF 2.5 ) Pub Date : 2022-06-23 , DOI: 10.1080/08916152.2022.2086323 Zhengping Zou 1, 2 , Yifan Wang 2 , Hui Li 2 , Yiming Chen 1, 2 , Lichao Yao 1, 2 , Huan Li 2 , Huoxing Liu 1, 2
Experimental Heat Transfer ( IF 2.5 ) Pub Date : 2022-06-23 , DOI: 10.1080/08916152.2022.2086323 Zhengping Zou 1, 2 , Yifan Wang 2 , Hui Li 2 , Yiming Chen 1, 2 , Lichao Yao 1, 2 , Huan Li 2 , Huoxing Liu 1, 2
Affiliation
The PCHE has been recognized as a promising heat exchanger for hypersonic precooled aero-engines due to its superior thermal performance, high compactness and robustness. The present work focuses o...
中文翻译：
高超声速预冷航空发动机锯齿形微通道PCHE的热工水力特性实验研究
PCHE 因其优越的热性能、高紧凑性和坚固性而被认为是高超音速预冷航空发动机的一种有前途的热交换器。目前的工作重点是...
更新日期：2022-06-23
中文翻译：
高超声速预冷航空发动机锯齿形微通道PCHE的热工水力特性实验研究
PCHE 因其优越的热性能、高紧凑性和坚固性而被认为是高超音速预冷航空发动机的一种有前途的热交换器。目前的工作重点是...
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