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1Design method for hypersonic bump inlet based on transverse pressure gradient
Author(s):Shang-cheng XU, Yi WANG, Zhen-guo ...  Clicked:1121  Download:1040  Cited:0  <Full Text>  <PPT> 267
Journal of Zhejiang University Science A  2022 Vol.23 No.6 P.479-494  DOI:10.1631/jzus.A2100532
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