Particle image velocimetry and a spectroscopy technique has been used to obtain information on the flow dynamics and flame thermal signatures of a fuel jet injected into a cross-flow of normal temperature and very high-temperature combustion air. Flame fluctuations were obtained using a high-speed camera and then performing fast Fourier transform on the signal. High-temperature air combustion has been demonstrated to provide significant energy savings, higher heat flux, and reduction of pollution and equipment size of industrial furnaces. The dynamics of flow associated with high temperature combustion air conditions (for mean velocity, axial strain rate and vorticity) has been obtained in two-dimensional using propane and methane as the fuels. The data have been compared with normal temperature combustion air case, including the nonburning case. A specially designed experimental test furnace facility was used to provide well-controlled conditions and allowed air preheats to using regenerative burners. Four different experimental cases have been examined. The momentum flux ratio between the burning and nonburning conditions was kept constant to provide comparison between cases. The results provide the role of high-temperature combustion air on the dynamics of the flow, turbulence, and mixing under nonburning and combustion conditions. The data provide the direct role of combustion on flow dynamics, turbulence, and flame fluctuations. High-temperature combustion air at low-oxygen concentration showed larger flame volume with less fluctuation than normal or high-temperature normal air cases. High-temperature combustion air technology prolongs mixing in the combustion zone to enhance the flame volume, reduce flame fluctuations, and to provide uniform flow and thermal characteristics. This information assists in model validation and model development for new applications and technology development using high-temperature air combustion principles.
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e-mail: akgupta@eng.umd.edu
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April 2007
Technical Papers
Experimental Investigation of Flow Phenomena of a Single Fuel Jet in Cross-Flow During Highly Preheated Air Combustion Conditions
Magnus Mörtberg,
Magnus Mörtberg
Department of Mechanical Engineering, The Combustion Laboratory,
University of Maryland
, College Park, MD 20742 and Department of Materials Science and Engineering, Division of Energy and Furnace Technology, Royal Institute of Technology (KTH)
, S10044, Stockholm, Sweden
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Wlodzimierz Blasiak,
Wlodzimierz Blasiak
Department of Mechanical Engineering, The Combustion Laboratory,
University of Maryland
, College Park, MD 20742 and Department of Materials Science and Engineering, Division of Energy and Furnace Technology, Royal Institute of Technology (KTH)
, S10044, Stockholm, Sweden
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Ashwani K. Gupta
Ashwani K. Gupta
Department of Mechanical Engineering, The Combustion Laboratory,
e-mail: akgupta@eng.umd.edu
University of Maryland
, College Park, MD 20742
Search for other works by this author on:
Magnus Mörtberg
Department of Mechanical Engineering, The Combustion Laboratory,
University of Maryland
, College Park, MD 20742 and Department of Materials Science and Engineering, Division of Energy and Furnace Technology, Royal Institute of Technology (KTH)
, S10044, Stockholm, Sweden
Wlodzimierz Blasiak
Department of Mechanical Engineering, The Combustion Laboratory,
University of Maryland
, College Park, MD 20742 and Department of Materials Science and Engineering, Division of Energy and Furnace Technology, Royal Institute of Technology (KTH)
, S10044, Stockholm, Sweden
Ashwani K. Gupta
Department of Mechanical Engineering, The Combustion Laboratory,
University of Maryland
, College Park, MD 20742e-mail: akgupta@eng.umd.edu
J. Eng. Gas Turbines Power. Apr 2007, 129(2): 556-564 (9 pages)
Published Online: May 28, 2006
Article history
Received:
October 22, 2004
Revised:
May 28, 2006
Citation
Mörtberg, M., Blasiak, W., and Gupta, A. K. (May 28, 2006). "Experimental Investigation of Flow Phenomena of a Single Fuel Jet in Cross-Flow During Highly Preheated Air Combustion Conditions." ASME. J. Eng. Gas Turbines Power. April 2007; 129(2): 556–564. https://doi.org/10.1115/1.2436558
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