Development of Emissions Measurement Techniques for Afterburning Turbine Engines

Abstract

Detailed emissions measurements were made throughout the plumes of J85-5 and J79-15 engines at military power and three afterburning power levels. Calculations of integrated pollutant flow rates at various axial stations showed that hydrocarbons are most reactive in the plume, with significant decreases observed at all afterburning power levels. Carbon monoxide can either increase or decrease with axial distance in the plume, depending on the power level and the hydrocarbon contents. No significant change in total oxides of nitrogen was observed at any power level. A computerized analytical plume model was developed and verified, which considers the simultaneous mixing and chemical reaction processes that can occur in the plumes of afterburning engines. The model enables calculating local concentrations of the various exhaust gases at any axial or radial location from initial values measured at the exhaust plane. A procedure for afterburning engine emissions measurements was developed.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1975
Accession Number
ADA019094

Entities

People

  • D. W. Bahr
  • M. J. Kenworthy
  • T. F. Lyon
  • W. C. Colley

Organizations

  • General Electric

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Force
  • Aircrafts
  • Boundary Layer
  • Chemical Kinetics
  • Chemical Reaction Properties
  • Chemical Reactions
  • Chemistry
  • Combustion
  • Combustion Products
  • Computational Fluid Dynamics
  • Computer Programs
  • Differential Equations
  • Exhaust Gases
  • Heat Transfer
  • Ignition Lag
  • Test Facilities
  • Turbines

Readers

  • Aerospace Propulsion Engineering.
  • Internal Combustion Engine (ICE) Technology.
  • Structural Dynamics.