THE EVALUATION OF A LIQUID METAL REGENERATOR FOR A 3750 HP TURBOPROP ENGINE

Abstract

The feasibility of a liquid metal heat exchange system as a versatile, high reliability component meeting the compactness and high performance characteristics required for the Navy's regenerative turboprop engine has been demonstrated.

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Document Details

Document Type
Technical Report
Publication Date
May 15, 1963
Accession Number
AD0407471

Entities

People

  • F. W. Saco
  • J. Horvath
  • L. R. Cox
  • R. Gill
  • R. Stevens

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Ground and Sea Platforms

DTIC Thesaurus Topics

  • Air Flow
  • Calorific Value
  • Combustion
  • Exhaust Gases
  • Fabrication
  • Gas Flow
  • Gas Turbines
  • Heat Energy
  • Heat Transfer
  • Liquid Metal Pumps
  • Liquid Metals
  • Mass Transfer
  • Materials
  • Test And Evaluation
  • Test Equipment
  • Turbines
  • Turboprop Engines

Readers

  • Aerospace Engineering
  • Combustion and Flow Dynamics.