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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

Crossref DOI link: https://doi.org/10.1007/s12206-022-0549-0

Published Online: 2022-06-20

Published Print: 2022-06

Update policy: https://doi.org/10.1007/springer_crossmark_policy

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