Enhancing the stability margin of single stage transonic axial flow compressor with bend skewed casing treatment (R)
Language: English Publication details: Bombay IIT 2015Description: xxiv,285 p. 30 cmSubject(s): Theses and Dissertations | Axial flow compressors -- Aerodynamics | Cascades(Fluid dynamics) | Numerical analysisDissertation note: Thesis Ph.D. Indian Institute of Technology Bombay. Department of Aeronautical Engineering 2015Item type | Current library | Call number | Status | Notes | Date due | Barcode | Item holds |
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Theses and Dissertations | Central Library, IITB Pamphlet Section (Theses, Standards, Reports) | 043:533.6.01:518.6 Alo | Not for loan | D07A04 | 238493 |
Total holds: 0
Thesis Ph.D. Indian Institute of Technology Bombay. Department of Aeronautical Engineering 2015
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