Laser-Based Investigations of Periodic Combustion Instabilities in a Gas Turbine Model CombustorSource: Journal of Engineering for Gas Turbines and Power:;2005:;volume( 127 ):;issue: 003::page 492DOI: 10.1115/1.1850498Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The driving mechanism of pulsations in gas turbine combustors depends on a complex interaction between flow field, chemistry, heat release, and acoustics. Experimental data on all these factors are therefore required to obtain insight into the coupling mechanisms during a pulsation period. In order to develop a comprehensive experimental database to support a phenomenological understanding and to provide validation data for numerical simulation, a standard burner for optical investigations was established that exhibits strong self-excited oscillations. The burner was a swirl-stabilized nonpremixed model combustor designed for gas turbine applications and operated using methane as fuel at atmospheric pressure. It was mounted in a combustion chamber, which provides almost unobstructed optical access. The periodic combustion instabilities were studied by a variety of phase-resolved laser-based diagnostic techniques, locked to the frequency of the dominant pressure oscillation. Measurement techniques used were LDV for velocity measurements, planar laser-induced fluorescence for imaging of CH and OH radicals, and laser Raman scattering for the determination of the major species concentrations, temperature, and mixture fraction. The phase-resolved measurements revealed significant variations of all measured quantities in the vicinity of the nozzle exit, which trailed off quickly with increasing distance. A strong correlation of the heat release rate and axial velocity at the nozzle was observed, while the mean mixture fraction as well as the temperature in the periphery of the flame is phase shifted with respect to axial velocity oscillations. A qualitative interpretation of the experimental observations is given, which will help to form a better understanding of the interaction between flow field, mixing, heat release, and temperature in pulsating reacting flows, particularly when accompanied by corresponding CFD simulations that are currently underway.
keyword(s): Oscillations , Pressure , Flow (Dynamics) , Heat , Temperature , Combustion , Lasers , Measurement , Combustion chambers , Gas turbines , Nozzles , Flames , Acoustics , Fuels , Mixtures , Mechanisms AND Computer simulation ,
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contributor author | R. Giezendanner | |
contributor author | B. Lehmann | |
contributor author | P. Weigand | |
contributor author | X. R. Duan | |
contributor author | W. Meier | |
contributor author | U. Meier | |
contributor author | M. Aigner | |
date accessioned | 2017-05-09T00:16:05Z | |
date available | 2017-05-09T00:16:05Z | |
date copyright | July, 2005 | |
date issued | 2005 | |
identifier issn | 1528-8919 | |
identifier other | JETPEZ-26871#492_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/131758 | |
description abstract | The driving mechanism of pulsations in gas turbine combustors depends on a complex interaction between flow field, chemistry, heat release, and acoustics. Experimental data on all these factors are therefore required to obtain insight into the coupling mechanisms during a pulsation period. In order to develop a comprehensive experimental database to support a phenomenological understanding and to provide validation data for numerical simulation, a standard burner for optical investigations was established that exhibits strong self-excited oscillations. The burner was a swirl-stabilized nonpremixed model combustor designed for gas turbine applications and operated using methane as fuel at atmospheric pressure. It was mounted in a combustion chamber, which provides almost unobstructed optical access. The periodic combustion instabilities were studied by a variety of phase-resolved laser-based diagnostic techniques, locked to the frequency of the dominant pressure oscillation. Measurement techniques used were LDV for velocity measurements, planar laser-induced fluorescence for imaging of CH and OH radicals, and laser Raman scattering for the determination of the major species concentrations, temperature, and mixture fraction. The phase-resolved measurements revealed significant variations of all measured quantities in the vicinity of the nozzle exit, which trailed off quickly with increasing distance. A strong correlation of the heat release rate and axial velocity at the nozzle was observed, while the mean mixture fraction as well as the temperature in the periphery of the flame is phase shifted with respect to axial velocity oscillations. A qualitative interpretation of the experimental observations is given, which will help to form a better understanding of the interaction between flow field, mixing, heat release, and temperature in pulsating reacting flows, particularly when accompanied by corresponding CFD simulations that are currently underway. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Laser-Based Investigations of Periodic Combustion Instabilities in a Gas Turbine Model Combustor | |
type | Journal Paper | |
journal volume | 127 | |
journal issue | 3 | |
journal title | Journal of Engineering for Gas Turbines and Power | |
identifier doi | 10.1115/1.1850498 | |
journal fristpage | 492 | |
journal lastpage | 496 | |
identifier eissn | 0742-4795 | |
keywords | Oscillations | |
keywords | Pressure | |
keywords | Flow (Dynamics) | |
keywords | Heat | |
keywords | Temperature | |
keywords | Combustion | |
keywords | Lasers | |
keywords | Measurement | |
keywords | Combustion chambers | |
keywords | Gas turbines | |
keywords | Nozzles | |
keywords | Flames | |
keywords | Acoustics | |
keywords | Fuels | |
keywords | Mixtures | |
keywords | Mechanisms AND Computer simulation | |
tree | Journal of Engineering for Gas Turbines and Power:;2005:;volume( 127 ):;issue: 003 | |
contenttype | Fulltext |