Boundary layer control during hypersonic shock-boundary layer interactions (R)
Material type: TextLanguage: English Publication details: Mumbai IIT 2022Description: xiv,106 p. 30 cmSubject(s): Theses and Dissertations | Aerospace engineering | Hypersonic flow | Hypersonic intakes | Shock boundary layer interactions | Flow control | Shock tunnelDissertation note: Thesis Ph.D. Indian Institute of Technology Bombay. Department of Aerospace Engineering. 2022Item type | Current library | Collection | Call number | Status | Date due | Barcode | Item holds |
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Theses and Dissertations | Central Library, IITB Pamphlet Section (Theses, Standards, Reports) | Reference | 533.6.07:629.136.2 Chi | Not for loan | 248871 |
Total holds: 0
Thesis Ph.D. Indian Institute of Technology Bombay. Department of Aerospace Engineering. 2022
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