The atomization characteristics of blends of bioderived camelina hydrogenated renewable jet (HRJ) alternative fuel with conventional aviation kerosene (Jet A-1) discharging into ambient atmospheric air from a dual-orifice atomizer used in aircraft engines are described. The spray tests are conducted in a spray test facility at six different test flow conditions to compare the atomization of alternative fuels with that of Jet A-1. The fuel sprays are characterized in terms of fuel discharge, spray cone angle, drop size distribution, and spray patternation. The measurements of spray drop size distribution are obtained using laser diffraction based Spraytec equipment. The characteristics of fuel discharge and cone angle of alternative fuel sprays do not show any changes from that of Jet A-1 sprays. The characteristics of spray drop size, evaluated in terms of the variation of mean drop size along the spray axis, for the alternative fuel sprays remain unaffected by the variation in fuel properties between the alternative fuels and Jet A-1. The measurements on spray patternation, obtained using a mechanical patternator at a distance 5.1 cm from the atomizer exit, show an enhanced fuel concentration in the vicinity of spray axis region for the alternative fuel sprays discharging from the dual-orifice atomizer.
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August 2015
Research-Article
Atomization Characteristics of Camelina-Based Alternative Aviation Fuels Discharging From Dual-Orifice Injector
D. Sivakumar,
D. Sivakumar
1
Associate Professor
Mem. ASME
Department of Aerospace Engineering,
e-mail: dskumar@aero.iisc.ernet.in
Mem. ASME
Department of Aerospace Engineering,
Indian Institute of Science
,Bangalore 560012
, India
e-mail: dskumar@aero.iisc.ernet.in
1Corresponding author.
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R. Sakthikumar,
R. Sakthikumar
Department of Aerospace Engineering,
e-mail: rcsakthikumar@gmail.com
Indian Institute of Science
,Bangalore 560012
, India
e-mail: rcsakthikumar@gmail.com
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B. N. Raghunandan,
B. N. Raghunandan
Professor
Department of Aerospace Engineering,
e-mail: raghubn@aero.iisc.ernet.in
Department of Aerospace Engineering,
Indian Institute of Science
,Bangalore 560012
, India
e-mail: raghubn@aero.iisc.ernet.in
Search for other works by this author on:
A. K. Jain
A. K. Jain
Search for other works by this author on:
D. Sivakumar
Associate Professor
Mem. ASME
Department of Aerospace Engineering,
e-mail: dskumar@aero.iisc.ernet.in
Mem. ASME
Department of Aerospace Engineering,
Indian Institute of Science
,Bangalore 560012
, India
e-mail: dskumar@aero.iisc.ernet.in
R. Sakthikumar
Department of Aerospace Engineering,
e-mail: rcsakthikumar@gmail.com
Indian Institute of Science
,Bangalore 560012
, India
e-mail: rcsakthikumar@gmail.com
B. N. Raghunandan
Professor
Department of Aerospace Engineering,
e-mail: raghubn@aero.iisc.ernet.in
Department of Aerospace Engineering,
Indian Institute of Science
,Bangalore 560012
, India
e-mail: raghubn@aero.iisc.ernet.in
John T. C. Hu
S. K. Puri
A. K. Jain
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 October 29, 2014; final manuscript received December 3, 2014; published online January 28, 2015. Editor: David Wisler.
J. Eng. Gas Turbines Power. Aug 2015, 137(8): 081503 (11 pages)
Published Online: August 1, 2015
Article history
Received:
October 29, 2014
Revision Received:
December 3, 2014
Online:
January 28, 2015
Citation
Sivakumar, D., Sakthikumar, R., Raghunandan, B. N., Hu, J. T. C., Puri, S. K., and Jain, A. K. (August 1, 2015). "Atomization Characteristics of Camelina-Based Alternative Aviation Fuels Discharging From Dual-Orifice Injector." ASME. J. Eng. Gas Turbines Power. August 2015; 137(8): 081503. https://doi.org/10.1115/1.4029426
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