A simple model for compressor stall cell propagationA simple model for full-span stall cells in axial compressors has been formulated. The sudden changes in velocity across blade rows as the blade passages enter and leave the stall are shown to have important dynamical consequences for the stall flow field. The one empirical constant needed in the analysis is determined using the data of Day (1976, 1978). From this, reasonable predictions of stall cell speed and trends in speed have been obtained for a number of different compressors. From the satisfactory comparison between predicted and measured stall cell speeds, it is tentatively concluded that the model contains the essentials of a correct description of the controlling mechanism of full-span rotating stall.
Document ID
19810045578
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cumpsty, N. A. (Cambridge University Cambridge, United Kingdom)
Greitzer, E. M. (MIT Cambridge, Mass., United States)
Date Acquired
August 11, 2013
Publication Date
March 1, 1981
Subject Category
Aerodynamics
Report/Patent Number
ASME PAPER 81-GT-73Report Number: ASME PAPER 81-GT-73
Meeting Information
Meeting: Gas Turbine Conference and Products Show
Location: Houston, TX
Start Date: March 9, 1981
End Date: March 12, 1981
Sponsors: American Society of Mechanical Engineers