Advances in Aerodynamics2025，Vol.7Issue(2)：P.1-22,22.DOI:10.1186/s42774-025-00206-7
Enhancement of scramjet inlet efficiency by geometrical modifications
Dinesh Kumar Bajaj 1Sakshi Tushar Kansara 1Nayani Kishore Nath 2Ashish Vashishtha 3Devabrata Sahoo4
作者信息
- 1. Department of Aerospace Engineering,School of Engineering and Sciences,MIT Art,Design and Technology University,Pune 412201,India
- 2. Advanced Systems Laboratory,Defence Research and Development Organization,Hyderabad 500058,India
- 3. Department of Aerospace and Mechanical Engineering,South East Technological University,Carlow R93 V960,Ireland
- 4. Department of Aerospace Engineering,Graphic Era(Deemed to Be University),Dehradun 248002,India
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摘要
关键词
Scramjets/Inlet-isolator/Flow control techniques/Passive boundary layer bleed/Lip-shock-induced separation/Total pressure recovery分类
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Dinesh Kumar Bajaj,Sakshi Tushar Kansara,Nayani Kishore Nath,Ashish Vashishtha,Devabrata Sahoo..Enhancement of scramjet inlet efficiency by geometrical modifications[J].Advances in Aerodynamics,2025,7(2):P.1-22,22.
