Measurements of aerodynamic damping on the MIT transonic rotor
February 1981
Main Author: | Crawley, Edward F. |
---|---|
Other Authors: | Massachusetts Institute of Technology. Gas Turbine and Plasma Dynamics Laboratory |
Format: | Technical Report |
Published: |
Cambridge, Mass. : Gas Turbine & Plasma Dynamics Laboratory, Massachusetts Institute of Technology, [1981]
2016
|
Subjects: | |
Online Access: | http://hdl.handle.net/1721.1/104728 |
Similar Items
-
Uniform-inlet three-dimensional transonic Beltrami flow through a ducted fan
by: Cheng, Wai Kong
Published: (2016) -
Exit flow from a transonic compressor rotor
by: Thompkins, William T., et al.
Published: (2016) -
Unconventional blade design for compressors
by: Gopalakrishnan, S.
Published: (2016) -
An experimental and computational study of the flow in a transonic compressor rotor
by: Thompkins, William T.
Published: (2016) -
Performance characteristics in transonic axial compressor rotor blade using circular jets
by: Epsipha, Pauline
Published: (2016)