Combustor Design Criteria Validation. Volume II. Development Testing of Two Full-Scale Annular Gas Turbine Combustors

Abstract

This report describes the development testing of two full-scale, reverse-flow, annular combustor systems that were designed based on the empirical/analytical design procedures described in Volume I. The baseline, Concept I, configuration met all design objectives with no hardware modifications. Concept II met the design objectives after only one major hardware modification design procedure for these two test concepts, the combustor-development time was significantly reduced, meeting the main objective of the USARTL Program. Volume III is the User's Manual for the models and includes a description of the models and a listing of the computer codes with instructions on usage.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1979
Accession Number
ADA067689

Entities

People

  • E. Coleman
  • H. Mongia
  • R. Reynolds
  • T. Bruce

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Pressure
  • Burning Rate
  • Combustion
  • Concept 1
  • Energy
  • Gas Turbines
  • Geometry
  • High Temperature
  • Ignition
  • Isotherms
  • Kinetic Energy
  • Measurement
  • Sea Level
  • Sound Pressure
  • Three Dimensional
  • Turbines
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Internal Combustion Engine (ICE) Technology.
  • Software Engineering