Report on a Special Gas Turbine Principle

Abstract

A special principle of gas turbines is described and investigated for aircraft application. A general description of this engine is provided, and an instructive picture of each individual process is disclosed. Test results already obtained are discussed. Suggestions are given for a testing program, and for a new test engine to be used in completing the previous test results.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1948
Accession Number
ADA800230

Entities

People

  • H. J. Pabst Von Ohain

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Flow
  • Air Force
  • Combustion
  • Combustion Chambers
  • Compressors
  • Gas Flow
  • Gas Turbines
  • Heat Energy
  • Heat Transfer
  • High Pressure
  • Jet Engines
  • Mechanical Energy
  • Shock Waves
  • Thermal Efficiency
  • Thermodynamic Processes
  • Turbines
  • Turbojet Engines

Readers

  • Aerospace Engineering
  • Theoretical Analysis.