Unsteady and Three-Dimensional Flow in Turbomachines.

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.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1996
Accession Number
ADA309985

Entities

People

  • A. H. Epstein
  • C. S. Tan
  • E. M. Greitzer
  • J. L. Kerrebrock

Organizations

  • Massachusetts Institute of Technology

Tags

Communities of Interest

  • Air Platforms
  • Human Systems
  • Space

DTIC Thesaurus Topics

  • Air Force
  • Boundary Layer
  • Computational Fluid Dynamics
  • Computational Science
  • Fluid Dynamics
  • Fluid Flow
  • Fluid Mechanics
  • Gas Turbines
  • Heat Transfer
  • Mechanical Phenomena
  • Physics Laboratories
  • Three Dimensional
  • Turbine Components
  • Turbines
  • Turbulent Mixing
  • Two Dimensional
  • Viscous Flow

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Combustion and Flow Dynamics.
  • Technical Research and Report Writing.