Evaluation of Future Jet Fuel Combustion Characteristics

Abstract

Future anticipated changes in jet fuel character can be expected to have substantial combustion system effects. This report contributes technical information to assist in future definition of new jet fuel specifications formulated with the intent of minimizing total cost of system operation while maintaining performance and flight safety. The impact of lower fuel hydrogen content on combustor liner temperatures, smoke, and gaseous emissions has been evaluated and improved correlations with hydrogen content have been developed. Results obtained with the various fuel blends tested have confirmed the dominant influence of hydrogen content on combustion characteristics when compared to volatility and hydrocarbon type effects. Use of the new non-dimensional liner temperature parameter has also resulted in a good correlation of a wide variety of previous combustor data involving rich combustion systems.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1978
Accession Number
ADA060218

Entities

People

  • T. A. Jackson
  • W. S. Blazowski

Organizations

  • Air Force Research Laboratory

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Space

DTIC Thesaurus Topics

  • Aircrafts
  • Chemistry
  • Combustion
  • Dielectric Gases
  • Exhaust Gases
  • Fuel Additives
  • Gas Turbines
  • Governments
  • Heat Transfer
  • High Pressure
  • Ignition
  • Jet Engine Fuels
  • Materials
  • Materials Laboratories
  • Materials Science
  • Measurement
  • Turbines

Fields of Study

  • Physics

Readers

  • Combustion science or combustion engineering.
  • Life Cycle Cost Analysis
  • Petroleum Engineering