Accession Number : ADA291275
Title : Characterization of Stall Inception in High-Speed Single-Stage Compressors.
Descriptive Note : Final rept. 1 Aug-1 Dec 92,
Corporate Author : WRIGHT RESEARCH AND DEVELOPMENT CENTER WRIGHT-PATTERSON AFB OH AERO PROPULSION AND POWER LAB
Personal Author(s) : Boyer, Keith
PDF Url : ADA291275
Report Date : DEC 1994
Pagination or Media Count : 166
Abstract : All aircraft gas turbine engines currently compromise compression system performance at some point(s) in their operating envelope to obtain 'adequate' stall margin. This work pursues the concept of active stall control to minirnize or eliminate this penalty, thereby improving the performance of any aircraft gas turbine engine.
Descriptors : *AIRCRAFT ENGINES, *GAS TURBINES, *STALLING, *CENTRIFUGAL COMPRESSORS, COMPRESSION, CONTROL, AVIATION SAFETY.
Subject Categories : Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE