Accession Number : ADA311100
Title : Broad-Based High Frequency Jet Engine Control.
Descriptive Note : Final rept. Oct 93-Jul 95,
Corporate Author : GEORGIA TECH RESEARCH CORP ATLANTA
Personal Author(s) : Prasad, J. V. ; Rivera, Carlos
PDF Url : ADA311100
Report Date : 22 JAN 1996
Pagination or Media Count : 63
Abstract : The focus of the effort being carried out under the AFOSR grant is to fully characterize the behavior of rotating stall phenomenon in turbomachinery systems and to assess effectiveness of nonlinear control strategies using both CFD simulations and experiments on the axial compressor facility in the LICCHUS lab. Toward accomplishing this objective, a CFD model has been developed and it has been validated using experimental data available in the literature. The axial compressor facility in the LICCHUS lab will be used for correlation with CFD simulations and for stall controller studies.
Descriptors : *AIRCRAFT ENGINES, *ENGINE COMPONENTS, *JET ENGINES, *STALLING, *ROTATION, *TURBOMACHINERY, CONTROL, HIGH FREQUENCY, EXPERIMENTAL DATA, COMPUTATIONAL FLUID DYNAMICS, NONLINEAR SYSTEMS, AXIAL FLOW COMPRESSORS.
Subject Categories : Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE