Characterization of wake- and tip-vortex-induced unsteady blade response in multistage compressor environment

Characterization of wake- and tip-vortex-induced unsteady blade response in multistage compressor environment

Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2002.

Bibliographic Details
Main Author: Lenglin, Geoffroy (Geoffroy Philippe), 1976-
Other Authors: Choon S. Tan.
Format: Thesis
Language:eng
Published: Massachusetts Institute of Technology 2013
Subjects:
Aeronautics and Astronautics.
Online Access:http://hdl.handle.net/1721.1/82227

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