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index	Title
1	Design method for hypersonic bump inlet based on transverse pressure gradient Author(s):Shang-cheng XU, Yi WANG, Zhen-guo ...  Clicked:2433  Download:1776  Cited:0  <Full Text>  <PPT> 617 Journal of Zhejiang University Science A  2022 Vol.23 No.6 P.479-494  DOI:10.1631/jzus.A2100532

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