Accession Number : ADP007692
Title : Application of CFD in the Design of Gas Turbine Engine Components,
Corporate Author : TEXTRON LYCOMING STRATFORD CT
Personal Author(s) : Sehra, Arun K. ; Abolfadl, Mohamed A. ; Zedan, Mohamed G.
Report Date : FEB 1992
Pagination or Media Count : 34
Abstract : The primary focus of this paper is to illustrate the application of three-dimensional viscous procedures for optimizing the turbomachinery component geometry. Specific cases presented in the paper include the application of three-dimensional viscous analyses to a transonic axial compressor rotor, a splittered axial compressor rotor, a turbine rotor, and an exhaust mixer-nozzle. Application of an axisymmetric Navier Stokes solver to the inlet particle separator, and a two-dimensional inverse design procedures for customizing compressor airfoil geometry are also briefly included.
Descriptors : *TURBOMACHINERY, *ENGINE COMPONENTS, *GAS TURBINES, AIRFOILS, AXISYMMETRIC, COMPRESSOR ROTORS, COMPRESSORS, GEOMETRY, INLETS, NOZZLES, PAPER, PARTICLES, ROTORS, SEPARATORS, THREE DIMENSIONAL, TURBINES, TWO DIMENSIONAL.
Subject Categories : Aerodynamics
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE