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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:2214  Download:1662  Cited:0  <Full Text>  <PPT> 583 Journal of Zhejiang University Science A  2022 Vol.23 No.6 P.479-494  DOI:10.1631/jzus.A2100532
2	Effects of bump parameters on hypersonic inlet starting performance Author(s):Shang-cheng XU, Yi WANG, Zhen-guo ...  Clicked:1196  Download:1032  Cited:0  <Full Text>  <PPT> 414 Journal of Zhejiang University Science A  2022 Vol.23 No.10 P.807-819  DOI:10.1631/jzus.A2200155

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