The effect of inlet pressure distortion on the performance of an axisymmetric compact tube heat exchanger with radial counter flow type for hypersonic pre-cooled aero-engine

标题
The effect of inlet pressure distortion on the performance of an axisymmetric compact tube heat exchanger with radial counter flow type for hypersonic pre-cooled aero-engine
作者
关键词
-
出版物
Journal of Mechanical Science and Technology
Volume 36, Issue 6, Pages 3181-3191
出版商
Springer Science and Business Media LLC
发表日期
2022-06-20
DOI
10.1007/s12206-022-0549-0

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