Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2009.Cataloged from PDF version of thesis.Includes bibliographical references (p. 133-135).The stable operation of centrifugal compressors is limited by well-known phenomena, rotating stall and surge. Although the manifestation of the full scale instabilities is similar to the ones observed in axial machines, the stall inception in centrifugal compressors is less well understood. This thesis focuses on developing an integrated methodology to predict the stability limit and the stall inception pattern in highly-loaded centrifugal compressors with vaned diffusers. The approach, based on a body force representation of the blade rows, is different from ...
This study concerns a 2.5 pressure ratio centrifugal compressor stage consisting of a splittered uns...
Recent studies showed that a prompt detection of the stall inception, connected with a specific mode...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2006.In...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2010.Th...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2007.Th...
This project is focused on modeling the internal flow in centrifugal compressors for the purpose of ...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2008.In...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2009.In...
A single stage industrial centrifugal compressor including vaneless diffuser and a non-symmetric vol...
High-speed centrifugal compressor requirements include a wide operating range between choking and st...
Recent studies showed that a prompt detection of the stall inception, connected with a specific mode...
Recent studies showed that a prompt detection of the stall inception, connected with a specific mode...
LecturePg. 71-82Techniques for rotating stall verification and analysis of detrimental effects are d...
Recent studies showed that a prompt detection of the stall inception, connected with a specific mode...
Recent studies showed that a prompt detection of the stall inception, connected with a specific mode...
This study concerns a 2.5 pressure ratio centrifugal compressor stage consisting of a splittered uns...
Recent studies showed that a prompt detection of the stall inception, connected with a specific mode...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2006.In...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2010.Th...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2007.Th...
This project is focused on modeling the internal flow in centrifugal compressors for the purpose of ...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2008.In...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2009.In...
A single stage industrial centrifugal compressor including vaneless diffuser and a non-symmetric vol...
High-speed centrifugal compressor requirements include a wide operating range between choking and st...
Recent studies showed that a prompt detection of the stall inception, connected with a specific mode...
Recent studies showed that a prompt detection of the stall inception, connected with a specific mode...
LecturePg. 71-82Techniques for rotating stall verification and analysis of detrimental effects are d...
Recent studies showed that a prompt detection of the stall inception, connected with a specific mode...
Recent studies showed that a prompt detection of the stall inception, connected with a specific mode...
This study concerns a 2.5 pressure ratio centrifugal compressor stage consisting of a splittered uns...
Recent studies showed that a prompt detection of the stall inception, connected with a specific mode...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2006.In...