The smoke point has been shown to be quantitatively related to the molecular structure of hydrocarbon fuels. A fast technique of determining the molecular composition of commercial and experimental fuels, in terms of carbon type structure, by using proton nuclear magnetic resonance (1H NMR) spectrometry, has been described. By measuring the smoke point soot yields of a laminar diffusion flame with a group of fuels—all having a constant hydrogen-to-carbon ratio—it has been shown that neither the smoke point nor the hydrogen-to-carbon ratio alone can describe the sooting propensity of turbine fuels. Obtained results indicate that smoke points and hydrogen-to-carbon ratio are complementary to each other in describing the sooting propensities of turbine fuels. This has been further tested using the available data in literature obtained from gas turbine combustors and diffusion flames.
Skip Nav Destination
Article navigation
January 1989
Research Papers
Effect of Molecular Structure on Soot Formation Characteristics of Aviation Turbine Fuels
O¨. L. Gu¨lder,
O¨. L. Gu¨lder
National Research Council of Canada, Division of Mechanical Engineering, Ottawa, Ontario K1A 0R6, Canada
Search for other works by this author on:
B. Glavincˇevski,
B. Glavincˇevski
National Research Council of Canada, Division of Mechanical Engineering, Ottawa, Ontario K1A 0R6, Canada
Search for other works by this author on:
S. Das
S. Das
Engine Laboratory, Indian Institute of Petroleum, Dehradun-248005, India
Search for other works by this author on:
O¨. L. Gu¨lder
National Research Council of Canada, Division of Mechanical Engineering, Ottawa, Ontario K1A 0R6, Canada
B. Glavincˇevski
National Research Council of Canada, Division of Mechanical Engineering, Ottawa, Ontario K1A 0R6, Canada
S. Das
Engine Laboratory, Indian Institute of Petroleum, Dehradun-248005, India
J. Eng. Gas Turbines Power. Jan 1989, 111(1): 77-83 (7 pages)
Published Online: January 1, 1989
Article history
Received:
September 1, 1987
Online:
October 15, 2009
Citation
Gu¨lder, O. L., Glavincˇevski, B., and Das, S. (January 1, 1989). "Effect of Molecular Structure on Soot Formation Characteristics of Aviation Turbine Fuels." ASME. J. Eng. Gas Turbines Power. January 1989; 111(1): 77–83. https://doi.org/10.1115/1.3240230
Download citation file:
Get Email Alerts
On Leakage Flows In A Liquid Hydrogen Multi-Stage Pump for Aircraft Engine Applications
J. Eng. Gas Turbines Power
A Computational Study of Temperature Driven Low Engine Order Forced Response In High Pressure Turbines
J. Eng. Gas Turbines Power
The Role of the Working Fluid and Non-Ideal Thermodynamic Effects on Performance of Gas Lubricated Bearings
J. Eng. Gas Turbines Power
Tool wear prediction in broaching based on tool geometry
J. Eng. Gas Turbines Power
Related Articles
Fuel Molecular Structure and Flame Temperature Effects on Soot Formation in Gas Turbine Combustors
J. Eng. Gas Turbines Power (January,1990)
Radiation and Smoke From the Gas Turbine Combustor Using Heavy Fuels
J. Heat Transfer (February,1983)
Soot Formation in a Turbulent Swirl Stabilized Laboratory Combustor
J. Eng. Power (January,1981)
Comparison of Filter Smoke Number and Elemental Carbon Mass From Partially Premixed Low Temperature Combustion in a Direct-Injection Diesel Engine
J. Eng. Gas Turbines Power (October,2011)
Related Proceedings Papers
Related Chapters
Combined Cycle Power Plant
Energy and Power Generation Handbook: Established and Emerging Technologies
Introduction
Nanomaterials in Glucose Sensing: Biomedical & Nanomedical Technologies - Concise Monographs
On Interfacial Ribbons of ζ- and γ-Hydride Phases Surrounding δ Precipitates in Zircaloy-2
Zirconium in the Nuclear Industry: 20th International Symposium