Multi-disciplinary design optimization (MDO) approach for launch vehicle conceptual design with concurrent optimization of vehicle and trajectory subsystems (R)
Language: English Publication details: Bombay IIT 2009Description: xiv,195 p. 30 cmSubject(s): Theses and Dissertations | Multidisciplinary design optimization | Launch vehicles(astronautics) | Space vehicles -- Aerodynamics | Mathematical optimizationDissertation note: Thesis Ph.D. Indian Institute of Technology Bombay. Department of Aeronautical Engineering 2009Item type | Current library | Call number | Status | Notes | Date due | Barcode | Item holds |
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Central Library, IITB Pamphlet Section (Theses, Standards, Reports) | 043:629.78:519.3 Gee | Not for loan | D07A03 | 223984 |
Total holds: 0
Thesis Ph.D. Indian Institute of Technology Bombay. Department of Aeronautical Engineering 2009
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