Heat Transfer Problems in Advanced Gas Turbines for Naval Applications.

Abstract

The report covers heat exchanger studies stressing measurements of local heat transfer coefficients. Direct heat transfer measurements have been performed and a method has also been used which is based on the heat and mass transfer analogy. Local ablation rates are obtained on a model covered with napthalene and heat transfer rates are deduced from these through the analogy. Measurements of the turbulence intensity in a gas stream leaving a combustion chamber are also reported. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Nov 30, 1978
Accession Number
ADA062866

Entities

People

  • E. M. Sparrow
  • E. R. G. Eckert
  • R. J. Goldstein

Organizations

  • University of Minnesota

Tags

Communities of Interest

  • Air Platforms
  • Ground and Sea Platforms

DTIC Thesaurus Topics

  • Boundary Layer
  • Combustion
  • Combustion Chambers
  • Combustors
  • Engineering
  • Gas Turbines
  • Heat Exchangers
  • Heat Transfer
  • Heat Transfer Coefficients
  • Mass Transfer
  • Measurement
  • Mechanical Engineering
  • Military Research
  • Pressure Distribution
  • Propulsion Systems
  • Reynolds Number
  • Thermodynamics

Readers

  • Fluid Dynamics.
  • Theoretical Analysis.
  • Thermal Physics or Thermal Science.