In the design of gas turbine combustors, efforts are engineered toward reducing the combustion pollutant emission levels. The pollutant emissions can be reduced by premixing the fuel and the air prior to ignition. However, the main challenges encountered with premixing are flame flashback and blowout, thus, the preference of diffusion flames. In this study, flame behavior, flow patterns, and thermochemical fields of backward-inclined diffusion jet flames in crossflow at low jet-to-crossflow momentum flux ratio of smaller than 0.04 were studied in a wind tunnel. The backward-inclination angle was varied within 0–50 deg. The flames presented three characteristic modes: crossflow dominated flame (low backward inclination angle) denoted by a large down-washed recirculation flame, transitional flame (mediate backward inclination angle) identified by a recirculation flame and a tail flame, and jet dominated flame (high backward inclination angle) characterized by a blue flame base, a yellow tail flame, and the absence of a recirculation flame. Short flames are detected in the regime of the crossflow dominated flames—an indication of improved fuel–air mixing. The findings suggest that for low exhaust emissions which are vigorously pursued in the aviation and thermal power plant industries, especially during low-load operations, the jet dominated flames are the preferable flames as they generate low unburned hydrocarbon, carbon monoxide, and nitric oxide emissions compared to the other flames.
Skip Nav Destination
Article navigation
Research-Article
Backward-Inclined Diffusion Jet Flames in Crossflow at Low Jet-to-Crossflow Momentum Flux Ratios
Dickson Bwana Mosiria,
Dickson Bwana Mosiria
Department of Mechanical Engineering,
National Taiwan University of Science and
Technology,
No. 43, Section 4, Keelung Road,
Taipei 10672, Taiwan, China
e-mail: dickson.bwana@yahoo.com
National Taiwan University of Science and
Technology,
No. 43, Section 4, Keelung Road,
Taipei 10672, Taiwan, China
e-mail: dickson.bwana@yahoo.com
Search for other works by this author on:
Rong Fung Huang,
Rong Fung Huang
Department of Mechanical Engineering,
National Taiwan University of Science and
Technology,
No. 43, Section 4, Keelung Road,
Taipei 10672, Taiwan, China
e-mail: rfhuang@mail.ntust.edu.tw
National Taiwan University of Science and
Technology,
No. 43, Section 4, Keelung Road,
Taipei 10672, Taiwan, China
e-mail: rfhuang@mail.ntust.edu.tw
Search for other works by this author on:
Ching Min Hsu
Ching Min Hsu
Department of Mechanical Design Engineering,
National Formosa University,
Huwei Township, Yunlin County,
Taiwan 63246,
e-mail: cmhsu@nfu.edu.tw
National Formosa University,
Huwei Township, Yunlin County,
Taiwan 63246,
e-mail: cmhsu@nfu.edu.tw
Search for other works by this author on:
Dickson Bwana Mosiria
Department of Mechanical Engineering,
National Taiwan University of Science and
Technology,
No. 43, Section 4, Keelung Road,
Taipei 10672, Taiwan, China
e-mail: dickson.bwana@yahoo.com
National Taiwan University of Science and
Technology,
No. 43, Section 4, Keelung Road,
Taipei 10672, Taiwan, China
e-mail: dickson.bwana@yahoo.com
Rong Fung Huang
Department of Mechanical Engineering,
National Taiwan University of Science and
Technology,
No. 43, Section 4, Keelung Road,
Taipei 10672, Taiwan, China
e-mail: rfhuang@mail.ntust.edu.tw
National Taiwan University of Science and
Technology,
No. 43, Section 4, Keelung Road,
Taipei 10672, Taiwan, China
e-mail: rfhuang@mail.ntust.edu.tw
Ching Min Hsu
Department of Mechanical Design Engineering,
National Formosa University,
Huwei Township, Yunlin County,
Taiwan 63246,
e-mail: cmhsu@nfu.edu.tw
National Formosa University,
Huwei Township, Yunlin County,
Taiwan 63246,
e-mail: cmhsu@nfu.edu.tw
1Corresponding author.
Contributed by the Combustion and Fuels Committee of ASME for publication in the JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER. Manuscript received March 11, 2018; final manuscript received October 25, 2018; published online November 19, 2018. Assoc. Editor: Eric Petersen.
J. Eng. Gas Turbines Power. May 2019, 141(5): 051501 (10 pages)
Published Online: November 19, 2018
Article history
Received:
March 11, 2018
Revised:
October 25, 2018
Citation
Mosiria, D. B., Huang, R. F., and Hsu, C. M. (November 19, 2018). "Backward-Inclined Diffusion Jet Flames in Crossflow at Low Jet-to-Crossflow Momentum Flux Ratios." ASME. J. Eng. Gas Turbines Power. May 2019; 141(5): 051501. https://doi.org/10.1115/1.4041870
Download citation file:
Get Email Alerts
Cited By
Inter-Stage Pressure Drop of Multi-Stage Brush Seal With Differentiated Structure
J. Eng. Gas Turbines Power (July 2023)
Estimation of Wiebe Function Parameters for Syngas and Anode Off-Gas Combustion in Spark-Ignition Engines
J. Eng. Gas Turbines Power (July 2023)
Mixture Distribution in Spark Ignited Port Fuel Injection Engines: A Review
J. Eng. Gas Turbines Power (July 2023)
Related Articles
Three-Stream Flamelet Model for Industrial Applications
J. Eng. Gas Turbines Power (June,2010)
Visualizing Diffusion Flame Formation in the Wake of Partially Premixed Combustion
J. Energy Resour. Technol (September,2001)
In Situ Detailed Chemistry Calculations in Combustor Flow Analyses
J. Eng. Gas Turbines Power (October,2001)
Two-Dimensional Spectroscopic Observation of Nonluminous Flames in a Regenerative Industrial Furnace Using Coal Gas
J. Eng. Gas Turbines Power (January,2004)
Related Proceedings Papers
Related Chapters
The Identification of the Flame Combustion Stability by Combining Principal Component Analysis and BP Neural Network Techniques
International Conference on Mechanical Engineering and Technology (ICMET-London 2011)
Assessment of Remote Cavitation Detection Methods with Flow Visualization in a Full Scale Francis Turbine
Proceedings of the 10th International Symposium on Cavitation (CAV2018)
In-Nozzle Flow Visualization of Marine Diesel Injector Nozzles with Different Inlet Radii
Proceedings of the 10th International Symposium on Cavitation (CAV2018)