Accession Number : ADA309985
Title : Unsteady and Three-Dimensional Flow in Turbomachines.
Descriptive Note : Final rept. 20 Oct 92-31 Oct 95,
Corporate Author : MASSACHUSETTS INST OF TECH CAMBRIDGE DEPT OF AERONAUTICS AND ASTRONAUTICS
Personal Author(s) : Greitzer, E. M. ; Epstein, A. H. ; Kerrebrock, J. L. ; Tan, C. S.
PDF Url : ADA309985
Report Date : MAR 1996
Pagination or Media Count : 59
Abstract : This report describes work carried out at the Gas Turbine Laboratory at MIT during the period 10/20/92 - 10/31/95, as part of a multi-investigator effort on unsteady and three-dimensional flow phenomena in turbomachines. Within the overall project, three separate tasks are specified. These are, in brief: 1. Characterization of Fully Scaled, Unsteady Film Cooled Turbine Blade Heat Transfer and Aerodynamics; 2. Flow Control in Compression Systems by Viscous Flow Removal; and 3. Unsteady Phenomena in Turbomachinery Endwall Flows.
Descriptors : *COMPUTATIONAL FLUID DYNAMICS, *GAS TURBINES, *UNSTEADY FLOW, *THREE DIMENSIONAL FLOW, HEAT TRANSFER, MATHEMATICAL MODELS, HIGH TEMPERATURE, DEFORMATION, DYNAMIC RESPONSE, SHOCK WAVES, EFFICIENCY, BOUNDARY LAYER, TURBULENCE, HIGH PRESSURE, VORTICES, COMPRESSIBLE FLOW, FLOW FIELDS, WAKE, GAS TURBINE BLADES, VISCOUS FLOW, HYDRODYNAMICS, FILM COOLING, INLETS, PRESSURE DISTRIBUTION, TURBOMACHINERY, AXIAL FLOW COMPRESSORS, BLADE TIPS.
Subject Categories : Fluid Mechanics
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE