Analysis of Effect of Basic Design Variables on Subsonic Axial-flow-compressor Performance
Author : John T. Sinnette (Jr.)
Publisher :
Page : pages
File Size : 47,4 MB
Release : 1948
Category :
ISBN :
Author : John T. Sinnette (Jr.)
Publisher :
Page : pages
File Size : 47,4 MB
Release : 1948
Category :
ISBN :
Author : John T. Sinnette
Publisher :
Page : 21 pages
File Size : 12,99 MB
Release : 1948
Category :
ISBN :
Author : John T. Sinnette (Jr.)
Publisher :
Page : 66 pages
File Size : 43,1 MB
Release : 1947
Category : Aeronautics
ISBN :
Author : Lewis Research Center
Publisher :
Page : 542 pages
File Size : 16,19 MB
Release : 1965
Category : Axial flow compressors
ISBN :
Author : Melvyn Savage
Publisher :
Page : 40 pages
File Size : 11,2 MB
Release : 1950
Category : Axial flow compressors
ISBN :
Multistage compressors composed of high-pressure-ratio stages have higher over-all off-design efficiencies and a wider operating range than those made up of low-pressure-ratio stages if the blade-row efficiency curves for the two cases are assumed to be somewhat similar.
Author : Robert O. Bullock
Publisher :
Page : 552 pages
File Size : 40,14 MB
Release : 1965
Category : Axial flow compressors
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 34 pages
File Size : 38,85 MB
Release : 1948
Category : Aeronautics
ISBN :
Author : George K. Serovy
Publisher :
Page : 42 pages
File Size : 15,95 MB
Release : 1959
Category : Mach number
ISBN :
Author :
Publisher :
Page : 460 pages
File Size : 20,98 MB
Release : 1950
Category : Aeronautics
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 1136 pages
File Size : 31,81 MB
Release : 1958
Category : Aeronautics
ISBN :