Effect of shock-induced flow separation in scramjet intake at flight conditions (R)
Material type:
TextLanguage: English Publication details: Bombay IIT 2020Description: xviii,148 p. 30 cmSubject(s): Theses and Dissertations | Airplanes -- Scramjet engines | Shock waves | Shock boundary layer interactions | Flight conditions | Hypersonic intakes | Turbulence -- Mathematical modelsDissertation note: Thesis Ph.D Indian Institute of Technology Bombay. Department of Aerospace Engineering
2020
| Item type | Current library | Collection | Call number | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|
Theses and Dissertations
|
Central Library, IITB Pamphlet Section (Theses, Standards, Reports) | Reference | 629.136.2 Sin | Not for loan | 247798 |
Total holds: 0
Thesis Ph.D Indian Institute of Technology Bombay. Department of Aerospace Engineering
2020
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