Active Control of Oscillations in Simulations of Gas-Turbine Combustors

Abstract

The approach to extinction of a premixed methane-air flame stabilized behind a plane sudden-expansion gave rise to cyclic movement of the position of flame stabilization with a period of the order of 100 ms. These oscillations have been quantified in terms of simultaneous measurements of pressure and light emission, and the pressure maximum corresponded to the flame position closest to the step and the minima to that furthest away. The active control strategy of imposing out-of-phase oscillations was unsuccessful since the period of the near-limit cycles varied over a substantial range and a new approach will be required to track the signal and to implement online actuation that will counteract the tendency for flame movement.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 2001
Accession Number
ADP011176

Entities

People

  • J. H. Uhm
  • J. H. Whitelaw
  • S. R. Dezilwa

Organizations

  • Imperial College London

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Amplitude
  • Combustion
  • Combustors
  • Control Systems
  • Flow Rate
  • Frequency
  • Gas Turbines
  • Mechanical Engineering
  • Military Aircraft
  • Pressure Transducers
  • Reynolds Number
  • Strain Rate
  • Transducers
  • Turbines
  • Turbulent Mixing
  • Vehicles

Fields of Study

  • Physics

Readers

  • Combustion science or combustion engineering.
  • Mathematics or Statistics
  • Robotics and Automation.