Studies of Gas Turbine Heat Transfer Airfoil Surface and End-Wall.

Abstract

This report documents work on the topic of heat transfer from gas turbine airfoil, end-wall and internal passage surfaces. The research is divided into the following subtopics: curvature effects, including transition and film cooling; and airfoil heat transfer, including portions near the endwall. Keywords: Cascade structures; End-all curvature.

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1987
Accession Number
ADA181558

Entities

People

  • Ernst R. Eckert
  • Richard J. Goldstein
  • Terrence W. Simon

Organizations

  • University of Minnesota

Tags

Communities of Interest

  • Air Platforms
  • Sensors

DTIC Thesaurus Topics

  • Boundary Layer
  • Computational Fluid Dynamics
  • Fluid Dynamics
  • Fluid Flow
  • Fluid Mechanics
  • Gas Turbines
  • Heat Transfer
  • Heat Transfer Coefficients
  • Hydrodynamics
  • Measurement
  • Mechanical Properties
  • Mechanics
  • Test Facilities
  • Turbines
  • Turbulent Flow
  • Turbulent Mixing
  • Two Dimensional

Fields of Study

  • Physics

Readers

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