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Control of shock wave-boundary layer interaction-induced separation in scramjet inlet isolator via fluid extraction: a numerical optimization study

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dc.contributor.author B., Neeraj
dc.contributor.author Aggarwal, Divyank
dc.contributor.author Bhardwaj, Harshvardhan
dc.date.accessioned 2025-06-05T06:28:53Z
dc.date.available 2025-06-05T06:28:53Z
dc.date.issued 2025-05
dc.identifier.citation Under the guidance of Dr. Kumar Gaurav, Project Supervisor, UPES and Dr. Ram Kunwar, Activity Coordinator, UPES en_US
dc.identifier.uri https://dr.ddn.upes.ac.in//xmlui/handle/123456789/4457
dc.description Submitted in the partial fulfillment of the requirement for the degree of B. Tech (Aerospace Engineering) en_US
dc.language.iso en en_US
dc.publisher School of Advanced Engineering, UPES, Dehradun en_US
dc.subject Dissertation en_US
dc.subject Aerospace Engineering en_US
dc.subject Hypersonic Inlet en_US
dc.title Control of shock wave-boundary layer interaction-induced separation in scramjet inlet isolator via fluid extraction: a numerical optimization study en_US
dc.type Other en_US


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