Control of Alternating Flow Phenomena in Transonic Shock Wave Boundary Layer Interactions Over Payload Region of a Generic Launch Vehicle Model

dc.contributor.guide	Suryanarayana, G K and Jagadeesh, G
dc.coverage.spatial
dc.creator.researcher	Singh, Dheerendra Bahadur
dc.date.accessioned	2025-12-11T05:45:27Z
dc.date.available	2025-12-11T05:45:27Z
dc.date.awarded	2025
dc.date.completed	2024
dc.date.registered	2014
dc.description.abstract	newline
dc.description.note
dc.format.accompanyingmaterial	DVD
dc.format.dimensions
dc.format.extent
dc.identifier.researcherid
dc.identifier.uri	http://hdl.handle.net/10603/679720
dc.language	English
dc.publisher.institution	Aerospace Engineering
dc.publisher.place	Bangalore
dc.publisher.university	Indian Institute of Science Bangalore
dc.relation
dc.rights	university
dc.source.university	University
dc.subject.keyword	Engineering
dc.subject.keyword	Engineering Aerospace
dc.subject.keyword	Engineering and Technology
dc.title	Control of Alternating Flow Phenomena in Transonic Shock Wave Boundary Layer Interactions Over Payload Region of a Generic Launch Vehicle Model
dc.title.alternative
dc.type.degree	Ph.D.