Author: Jacques ValensiPublisher:
ISBN:
Category :
Languages : en
Pages : 19
Book Description
Experimental Investigation of the Rotating Stall in a Single Stage Axial Compressor
Author: Jacques ValensiExperimental and Theoretical Investigation of Rotating-stall Characteristics of Single-stage Axial-flow Compressor with Hub-tip Ratio of 0.76
Author: Robert W. GrahamFront Stage Axial Compressor Stable Rotating Stall
Author: John P. D'AntonioThe Variational Analysis of the Rotating Stall and Its Experimental Investigation in the Axial-Flow Compressor
Author: Labib Mohamed Abd El-EzizPublisher:
ISBN:
Category :
Languages : en
Pages : 12
Book Description
Analytical and Experimental Investigation of Rotating Stall Phenomena in Turbine Engine Compressors
Author: Experimental Investigation of the Stalled Flow of a Single Stage Axial Compressor
Author: M. D. WoodPre-conference Reports
Author: Rotating Stall Investigation of the 0.72 Hub-tip Ratio Single-stage Compressor
Author: Robert W. GrahamPublisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 30
Book Description
Investigation of Rotating Stall in a Single Stage Axial Compressor
Author: Massachusetts Institute of Technology. Gas Turbine LaboratoryPublisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 31
Book Description
Investigation of Rotating Stall in a Single-stage Axial Compressor
Author: S. R. MontgomeryPublisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 28
Book Description
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.