The Use of Vortex Generators as Inexpensive Compressor Casing Treatment

760925

02/01/1976

Event
Aerospace Engineering and Manufacturing Meeting
Authors Abstract
Content
This paper describes an inexpensive form of casing treatment which was found to increase both efficiency and stall margin in an axial compressor stage and which could be easily and cheaply retrofitted to existing engines. The method consists of placement of a row of vortex generators on the outer casing of an axial compressor, upstream of the rotor. Design techniques are described. An experimental investigation is also described in which vortex generator tip treatment was applied to a single stage axial compressor. Gains in compressor efficiency and stall margin were observed.
Meta TagsDetails
DOI
https://doi.org/10.4271/760925
Pages
8
Citation
Law, C., Wennerstrom, A., and Buzzell, W., "The Use of Vortex Generators as Inexpensive Compressor Casing Treatment," SAE Technical Paper 760925, 1976, https://doi.org/10.4271/760925.
Additional Details
Publisher
Published
Feb 1, 1976
Product Code
760925
Content Type
Technical Paper
Language
English