Enhancing the stability margin of single stage transonic axial flow compressor with bend skewed casing treatment (R)

By: Alone, Dilipkumar Bhanudasji [Author]Contributor(s): Pradeep, A.M [Supervisor] | Ramamurthy, S [Supervisor] | Iyengar,Venkat S | Indian Institute of Technology Bombay Department of Aeronautical EngineeringLanguage: 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 2015
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Holdings
Item type Current library Call number Status Notes Date due Barcode Item holds
Theses and Dissertations 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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