INTERNATIONAL PROPULSION SYMPOSIUM, 1967, THE COLLEGE OF AERONAUTICS, CRANFIELD, ENGLAND.

Abstract

Contents: Requirements in Aircraft Gas Turbine Combustion Systems, Combustion in Industrial Gas Turbines, Combustion Development on the Rolls Royce Spey Engine, The Effect of Local Fuel Concentration on Reheat Jet Pipe Vibrations, Augmentation Systems for Turbofan Engines, Factors Controlling Gas Turbine Combustion Performance at High Pressure, A Review of Aero Engine Smoke Emission.

Document Details

Document Type
Technical Report
Publication Date
Aug 14, 1967
Accession Number
AD0820336

Entities

People

  • Harold L. Seligmiller

Organizations

  • Office of Naval Research

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Combustion
  • Engines
  • Gas Turbines
  • High Pressure
  • Ignition
  • Ignition Lag
  • Turbines
  • Turbofan Engines

Fields of Study

  • Physics

Readers

  • Academic Conference Management
  • Aerospace Engineering
  • Internal Combustion Engine (ICE) Technology.