THE INVESTIGATION OF A RESONANT WAVE ENGINE

Abstract

This report summarizes theoretical and experimental Investigations of a new font of intermittent heat engine employing pressure waves for compression prior to heat addition, which were carried oat at Cornell Aeronautical Laboratory between november 1951 and November 1955.

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1956
Accession Number
AD0129618

Entities

People

  • A. Hertzberg
  • A. L. Russo
  • J. G. Logan

Organizations

  • Calspan

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Combustion
  • Combustion Chambers
  • Computational Fluid Dynamics
  • Energy Transfer
  • Exhaust Gases
  • Fuel Injection
  • Fuel Injectors
  • Gas Turbines
  • Heat Engines
  • Heat Transfer
  • High Pressure
  • Ignition Systems
  • Jet Engines
  • Mach Number
  • Measurement
  • Test Beds
  • Turbojet Engines

Readers

  • Aerospace Engineering
  • Combustion Dynamics and Shock Wave Physics.
  • Technical Research and Report Writing.