Stall inception in axial flow compressors
Journal Article
·
· Journal of Turbomachinery; (United States)
- Cambridge Univ., Cambridge (United Kingdom). Engineering Dept.
Studies have been conducted on two laboratory test compressors to investigate the process leading to the formation of finite amplitude rotating stall cells. The measurements were obtained from circumferential arrays of hot wires and were spatially and temporarily analyzed to show that modal perturbations are not always present prior to stall, and when present, sometimes have little direct effect on the formation of the stall cells. The measurements lead to the conclusion that the occurrence of modal perturbations, and the formation of finite amplitude stall cells, are two separate phenomena, both occurring under roughly the same conditions at the peak of the pressure rise characteristic. The measurements also underline the hitherto unsuspected importance of short length scale disturbances in the process of stall inception. Examples are given of different ways in which stall cells can develop and the conclusions are backed up with a summary of current test data from various machines around the world.
- OSTI ID:
- 5878513
- Journal Information:
- Journal of Turbomachinery; (United States), Journal Name: Journal of Turbomachinery; (United States) Vol. 115:1; ISSN JOTUEI; ISSN 0889-504X
- Country of Publication:
- United States
- Language:
- English
Similar Records
Stall inception measurements in a high-speed multistage compressor
Stall inception and the prospects for active control in four high-speed compressors
Stall inception in the compressor system of a turbofan engine
Journal Article
·
Tue Oct 01 00:00:00 EDT 1996
· Journal of Turbomachinery
·
OSTI ID:404407
Stall inception and the prospects for active control in four high-speed compressors
Journal Article
·
Thu Dec 31 23:00:00 EST 1998
· Journal of Turbomachinery
·
OSTI ID:330486
Stall inception in the compressor system of a turbofan engine
Journal Article
·
Fri Dec 31 23:00:00 EST 1999
· Journal of Turbomachinery
·
OSTI ID:20020624