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

Internet

http://hdl.handle.net/1721.1/82227