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Please use this identifier to cite or link to this item: https://dr.ddn.upes.ac.in//xmlui/handle/123456789/4457
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dc.contributor.authorB., Neeraj-
dc.contributor.authorAggarwal, Divyank-
dc.contributor.authorBhardwaj, Harshvardhan-
dc.date.accessioned2025-06-05T06:28:53Z-
dc.date.available2025-06-05T06:28:53Z-
dc.date.issued2025-05-
dc.identifier.citationUnder the guidance of Dr. Kumar Gaurav, Project Supervisor, UPES and Dr. Ram Kunwar, Activity Coordinator, UPESen_US
dc.identifier.urihttps://dr.ddn.upes.ac.in//xmlui/handle/123456789/4457-
dc.descriptionSubmitted in the partial fulfillment of the requirement for the degree of B. Tech (Aerospace Engineering)en_US
dc.language.isoenen_US
dc.publisherSchool of Advanced Engineering, UPES, Dehradunen_US
dc.subjectDissertationen_US
dc.subjectAerospace Engineeringen_US
dc.subjectHypersonic Inleten_US
dc.titleControl of shock wave-boundary layer interaction-induced separation in scramjet inlet isolator via fluid extraction: a numerical optimization studyen_US
dc.typeOtheren_US
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