A computational investigation of the effects of inlet flow conditions on vaned diffuser performance
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997.
Main Author: | Phillips, Michael Stephen |
---|---|
Other Authors: | Choon S. Tan. |
Format: | Thesis |
Language: | eng |
Published: |
Massachusetts Institute of Technology
2010
|
Subjects: | |
Online Access: | http://hdl.handle.net/1721.1/50299 |
Similar Items
-
Role of flow alignment and inlet blockage on vaned diffuser performance
by: Phillips, Michael Stephen
Published: (2016) -
The role of impeller outflow conditions on the performance and stability of airfoil vaned radial diffusers
by: Everitt, Jonathan (Jonathan Neil)
Published: (2014) -
Aerodynamic design of moveable inlet guide vanes for active control of rotating stall
by: Silkowski, Peter D. (Peter Daniel)
Published: (2008) -
Enhanced compressor distortion tolerance using asymmetric inlet guide vane stagger
by: Schulmeyer, Andreas
Published: (2008) -
Investigation on inlet and entry region characteristics on the discrete passage diffuser pressure rise performance
by: Liang, Yongcheng
Published: (2009)