Secondary flow, total pressure loss and the effect of circumferential distortions in axial turbine cascades
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991.
Main Author: | Renaud, Earl William |
---|---|
Other Authors: | C.S. Tan. |
Format: | Thesis |
Language: | eng |
Published: |
Massachusetts Institute of Technology
2008
|
Subjects: | |
Online Access: | http://hdl.handle.net/1721.1/43059 |
Similar Items
-
An experimental investigation of the effects of inlet circumferential temperature distortion on the aerodynamic performance of a single stage turbine
by: Sujudi, David D. (David Dewantara)
Published: (2005) -
Impact of unsteady secondary air flow interaction with main flow on loss generation in axial turbines
by: Clifton, David (David Madison)
Published: (2015) -
Effect of circumferential groove casing treatment parameters on axial compressor flow range
by: Hanley, Brian K. (Brian Kyle)
Published: (2010) -
Secondary air interaction with main flow in axial turbines
by: Zlatinov, Metodi B. (Metodi Blagoev)
Published: (2011) -
Loss mechanisms in a highly loaded transonic axial turbine stage
by: Shannon, Kevin R. (Kevin Robert)
Published: (2019)