Stalled flow performance of a single stage transonic compressor
Name
06550418.pdf
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2.68 MB
Format
Adobe PDF
Checksum (MD5)
191bd5fb0e0a7bec1d4edb30f40862f7
Author(s)
Bartlett, Frederick Girard
Greitzer, E. M. (Edward M.), 1941-
Date Issued
1978
Publisher
Cambridge, Mass. : Massachusetts Institute of Technology, Gas Turbine & Plasma Dynamics Laboratory, [1978]
Series/Report no.
GT & PDL report ; no. 144
Abstract
The stalled flow performance of a single stage transonic compressor is examined, using data from the MIT Gas Turbine Laboratory's Blowdown Compressor Facility. Measurements of the blowdown corrected weightflow are included, as well as stage exit static to inlet total pressure rise, and rotating stall cell measurements. A comparison of the flow blockage, as represented by stall cell circumferential extent, with the blowdown corrected weightflow is made. The 100% design speed stalled flow performance characteristic is presented. Radial traverse.data is also presented including flow angles, static and total pressures, and Mach number components.
Description
Originally presented as the first author's thesis, M.S. in the M.I.T. Dept. of Mechanical Engineering, 1978
Includes bibliographical references (page 48)
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