A STUDY OF THE LOCAL HEAT TRANSFER OF A GAS-TURBINE PROFILE

Abstract

An experimental study was made of the heat transfer of a gas-turbine blade in a flat profile lattice with the maximum M number at the output of the lattice being M = 0.72. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jun 07, 1962
Accession Number
AD0286138

Entities

People

  • G.s. Ambrok

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Energy Generators
  • Energy Systems
  • Gas Turbine Blades
  • Gas Turbines
  • Generators
  • Heat Transfer
  • Mechanical Equipment
  • Rotor Blades (Turbomachinery)
  • Turbine Blades
  • Turbine Components
  • Turbines
  • Turbomachinery

Fields of Study

  • Engineering
  • Physics

Readers

  • Quantum spin resonance or Electron Paramagnetic Resonance spectroscopy.
  • Thermal Physics or Thermal Science.
  • Tribology (the study of the boundary interaction between sliding surfaces, lubrication, wear and friction).