Improved Correlations for Augmentor Static Stability (Postprint)

Abstract

Flame stability is critical to the operational performance of combustion systems in propulsion and power generation. Current predictive tools for flame stability are based on decades-old empirical correlations that have limited applicability for modern combustor designs. Recent advances in computational fluid dynamics (CFD) and advanced combustion diagnostics have provided new insight into the fundamental processes that occur in these flows. Reacting-flow CFD has yet to mature to a level where it can be practically applied as a design tool for this problem. This paper describes a new methodology for analyzing flame stability intended to provide designers with a significantly improved near-term predictive capability. Our predictive methodology is based on a Damk?hler number (Da) approach. Simplified CFD calculations are used to calculate relevant flow timescales, and reactor model calculations are used to characterize the important chemical timescales in the system. These timescales are used to form a Da number that is used to determine stability.

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 2007
Accession Number
ADA473730

Entities

People

  • Barry V. Kiel
  • Darin A. Knaus
  • Patrick J. Magari
  • Roger W. Hill
  • Scott D. Phillips

Organizations

  • Air Force Research Laboratory

Tags

Communities of Interest

  • Energy and Power Technologies
  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Afterburners
  • Air Force
  • Air Force Research Laboratories
  • Combustion
  • Combustors
  • Computational Fluid Dynamics
  • Dynamics
  • Fluid Dynamics
  • Fluid Flow
  • Gas Turbines
  • Ignition
  • Ignition Lag
  • Large Eddy Simulation
  • Mechanical Properties
  • Physics Laboratories
  • Turbines
  • Turbulent Mixing

Fields of Study

  • Engineering

Readers

  • Combustion and Flow Dynamics.
  • Combustion science or combustion engineering.
  • Systems Analysis and Design