Comparative study of tip clearance effects in compressors and turbines
May 1961
Main Author: | Yokoyama, Eiji |
---|---|
Other Authors: | Massachusetts Institute of Technology. Gas Turbine Laboratory |
Format: | Technical Report |
Published: |
Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1961]
2016
|
Subjects: | |
Online Access: | http://hdl.handle.net/1721.1/104710 |
Similar Items
-
Boundary layer effects on airfoil lift
by: Schneider, Kurt H. (Kurt Herbert)
Published: (2016) -
Lifting-line theory for subsonic axial compressor rotors
by: McCune, James E. (James Elliot), et al.
Published: (2016) -
Parametric dependencies of aeroengine flutter for flutter clearance applications
by: Khalak, Asif, 1972-
Published: (2016) -
Exit flow from a transonic compressor rotor
by: Thompkins, William T., et al.
Published: (2016) -
An experimental and computational study of the flow in a transonic compressor rotor
by: Thompkins, William T.
Published: (2016)