Experimental Investigation of the Rotating Stall in a Single Stage Axial Compressor
Author : Jacques Valensi
Publisher :
Page : 19 pages
File Size : 40,30 MB
Release : 1957
Category :
ISBN :
Author : Jacques Valensi
Publisher :
Page : 19 pages
File Size : 40,30 MB
Release : 1957
Category :
ISBN :
Author : Robert W. Graham
Publisher :
Page : 34 pages
File Size : 38,93 MB
Release : 1953
Category :
ISBN :
Author : John P. D'Antonio
Publisher :
Page : 140 pages
File Size : 47,89 MB
Release : 2015
Category :
ISBN :
Author : Labib Mohamed Abd El-Eziz
Publisher :
Page : 12 pages
File Size : 44,63 MB
Release : 1977
Category :
ISBN :
Author :
Publisher :
Page : 170 pages
File Size : 24,22 MB
Release : 1967
Category : Compressors
ISBN :
Author : M. D. Wood
Publisher :
Page : pages
File Size : 35,77 MB
Release : 1955
Category :
ISBN :
Author :
Publisher :
Page : 45 pages
File Size : 43,37 MB
Release : 1916*
Category : Missions
ISBN :
Author : Robert W. Graham
Publisher :
Page : 30 pages
File Size : 39,59 MB
Release : 1954
Category : Axial flow compressors
ISBN :
Author : Massachusetts Institute of Technology. Gas Turbine Laboratory
Publisher :
Page : 31 pages
File Size : 43,71 MB
Release : 1955
Category : Mechanical engineering
ISBN :
Author : S. R. Montgomery
Publisher :
Page : 28 pages
File Size : 33,2 MB
Release : 1957
Category : Axial flow compressors
ISBN :
The rotating-stall characteristics of a single-stage axial-flow compressor were investigated. The number of stall cells and their propagation velocities were found with and without stator blades. The measured velocities were compared with those predicted by Stenning's theory (see NACA TN 3580), assuming the dounstream pressure fluctuations to be negligible, and correlation within 10 percent was obtained at the onset of stall. It was found that the pressure fluctuations cauased by rotating stall were less downstream of the rotor than upstream; the minimum reduction across the rotor was 40 percent with stator blades and 75 percent without stator blades. It was also that, for the compressor tested, the stator blades decreased the number of stall cells and tended to induce rotating stall at larger mass flow rates.