A computational model for rotating stall and inlet distortions in multistage compressors

A computational model for rotating stall and inlet distortions in multistage compressors

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Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1999.

Bibliographic Details
Main Author: Gong, Yifang, 1964-
Other Authors: Choon Sooi Tan.
Format: Thesis
Language:eng
Published: Massachusetts Institute of Technology 2005
Subjects:
Aeronautics and Astronautics
Online Access:http://hdl.handle.net/1721.1/9733

Internet

http://hdl.handle.net/1721.1/9733

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