Rotating Stall Investigation of the 0.72 Hub-tip Ratio Single-stage Compressor
Author : Robert W. Graham
Publisher :
Page : 30 pages
File Size : 40,77 MB
Release : 1954
Category : Axial flow compressors
ISBN :
Author : Robert W. Graham
Publisher :
Page : 30 pages
File Size : 40,77 MB
Release : 1954
Category : Axial flow compressors
ISBN :
Author : Robert W. Graham
Publisher :
Page : 34 pages
File Size : 22,49 MB
Release : 1953
Category :
ISBN :
Author : Kjell Isaksen
Publisher :
Page : 146 pages
File Size : 29,33 MB
Release : 1957
Category :
ISBN :
Author : Eleanor L. Costilow
Publisher :
Page : 52 pages
File Size : 50,38 MB
Release : 1956
Category : Compressors
ISBN :
The rotating stall characteristics of several guide-vane - rotor and guide-vane - rotor - stator configurations were investigated. Guide vanes having turning angles of -22.5, 0 , 22.5, and 40 degrees were used. The stage hub-tip ratio was 0.9.
Author :
Publisher :
Page : 598 pages
File Size : 44,36 MB
Release : 1957
Category : Mechanics, Analytic
ISBN :
Author : J. Dunham
Publisher :
Page : 46 pages
File Size : 18,15 MB
Release : 1965
Category : Compressors
ISBN :
Author : Jacques Valensi
Publisher :
Page : 19 pages
File Size : 47,11 MB
Release : 1957
Category :
ISBN :
Author : United States. National Aeronautics and Space Administration
Publisher :
Page : pages
File Size : 44,28 MB
Release : 1960-07
Category :
ISBN :
Author :
Publisher :
Page : 288 pages
File Size : 26,21 MB
Release : 1965
Category : Mechanical engineering
ISBN :
Author : Massachusetts Institute of Technology. Gas Turbine Laboratory
Publisher :
Page : 31 pages
File Size : 10,8 MB
Release : 1955
Category : Mechanical engineering
ISBN :