Experimental Studies on Micro-Vortex Generator Controlled Shock/Boundary-Layer Interactions in Mach 2.2 Intake

Springer Science and Business Media LLC - Tập 20 Số 3 - Trang 584-595 - 2019
Mrinal Kaushik1
1Department of Aerospace Engineering, Indian Institute of Technology, Kharagpur, Kharagpur, India

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