Control of shock wave-boundary layer interaction-induced separation in scramjet inlet isolator via fluid extraction: a numerical optimization study
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School of Advanced Engineering, UPES, Dehradun
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Submitted in the partial fulfillment of the requirement for the degree of B. Tech (Aerospace Engineering)
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Under the guidance of Dr. Kumar Gaurav, Project Supervisor, UPES and Dr. Ram Kunwar, Activity Coordinator, UPES