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51	An experimental investigation of turbocharger stall Capece, Vincent Ralph January 1982 (has links) Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1982. / MICROFICHE COPY AVAILABLE IN ARCHIVES AND ENGINEERING. / Bibliography: leaves 47-49. / by Vincent Ralph Capece. / M.S. Mechanical Engineering. Superchargers Compressors Performance
52	Improving heat pump performance via compressor capacity control : analysis and test. Hiller, Carl Clifford January 1976 (has links) Thesis. 1976. Ph.D.--Massachusetts Institute of Technology. Dept. of Mechanical Engineering. / Microfiche copy available in Archives and Engineering. / Vita. / Includes bibliographical references. / Ph.D. Mechanical Engineering Compressors Heat pumps
53	Numerical prediction of the impact of non-uniform leading edge coatings on the aerodynamic performance of compressor airfoils / Elmstrom, Michael E. January 2004 (has links) (PDF) Thesis (M.S. in Mechanical Engineering)--Naval Postgraduate School, June 2004. / Thesis advisor(s): Knox Millsaps. Includes bibliographical references (p. 69-72). Also available online.
54	Nonlinear dynamic analysis and control of surge and rotating stall in axial compression systems Badmus, Olanrewju O. 05 1900 (has links) No description available. Compressors Structural dynamics Control theory
55	A numerical solution of implicit nonlinear equations of motion for rotor blades Kim, Young K. 12 1900 (has links) No description available. Compressors Blades Rotors (Helicopters) Aerodynamics
56	Inverse methodology for multi-point aerodynamic rotor blade design Tapia, Fidencio 05 1900 (has links) No description available. Compressors Blades Rotors Helicopters Aerodynamics
57	The efficiency of a viscous flow compressor Caldwell, John Spencer 08 1900 (has links) No description available. Compressors Design and construction Sealing (Technology)
58	A two-dimensional model to predict rotating stall in axial-flow compressors / Nowinski, Matthew C., January 1993 (has links) Thesis (M.S.)--Virginia Polytechnic Institute and State University, 1993. / Vita. Abstract. Includes bibliographical references (leaves 99-102). Also available via the Internet.
59	Spanwise mixing in multi-stage axial compressors Gallimore, Simon John January 1986 (has links) No description available. 532 Gas flow in axial compressors
60	Identification and Evaluation of Loss and Deviation Models for use in Transonic Compressor Stage Performance Prediction Cahill, Joseph E. 30 October 1997 (has links) The correlation of cascade experimental data is one method for obtaining compressor stage characteristics. These correlations specify pressure loss and flow turning caused by the blades. Current open literature correlations used in streamline curvature codes are inadequate for general application to high-speed transonic axial-flow compressors. The objective of this research was to investigate and evaluate the available correlations and ultimately discover sets of correlations which best fit the empirical data to be used in streamline curvature codes. Correlations were evaluated against experimental data from NASA Rotor 1-B and NASA Stage 35. It was found that no universal set of correlations was valid for minimum-loss point predictions. The Bloch shock loss model showed promising results in the stall regime for supersonic relative inlet Mach numbers. The Hearsey and Creveling off-minimum-loss deviation angle prediction performed consistently better than all other correlations tested. / Master of Science Axial Compressors Deviation Loss Transonic

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