Study the Effect of Air Pulsation on the Flame Characteristics
DOI:
https://doi.org/10.13052/ejcm2642-2085.29235Keywords:
Pulsating combustion, CFD, Pulsating flames, Detached eddy simulation (DES)Abstract
Pulsating combustion is used in a lot of industrial applications like conveyer drying, spray, boilers of commercial scale because its great role in increasing combustion efficiency and producing environmentally friendly combustion products. This paper evaluates how different frequencies (100, 200, 300, 400 and 500) rad/s applied to air velocity view a lot of improvements in the combustion and flow variables (v, T, NO and turbulent kinetic energy) and the effect of adding cross excess air to air pulsation with 500 rad/s frequency on the same flow variables. The performance of pulsating flames was numerically modulated by using Ansys Fluent 16 commercial package by building a 2D combustion chamber of Harwell standard furnace boundary condition on Ansys geometry and divided it into 61000 elements in Ansys meshing 16. Eddy Dissipation Model (EDM) is used to solve transient numerical combustion equations and Detached Eddy Simulation (DES) as viscous model. Converged numerical results have shown that increasing frequency from 100 to 500 rad/s increase average velocities of combustion products and turbulent kinetic energy by 22% and 80 respectively. The pollutant NO decrease by 60% and the time average temperature decrease from 1900 k to 1000 k.
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Shell, Royal Dutch. Shell Energy Scenarios 2050, Shell International BV. 2008.
Seyboth, Kristin, et al. Recognising the potential for renewable energy heating and cooling. Energy Policy. 2008; 36.7: 2460–2463.
Scotti, Alberto; Piomelli, Ugo. Turbulence models in pulsating flows. AIAA journal. 2002; 40.3: 537–544.
Valaev, Alexandr Alexandrovich, Dmitry Georgievich Zhimerin, Eduard Alexandrovich Mironov, and Vladimir Andreevich Popov. “Method and apparatus for intermittent combustion.” U.S. Patent 3,954,380, issued May 4, 1976.
Fureby, C., Lundgren, E. One-dimensional models for pulsating combustion. Combustion science and technology. 1993; 94.1–6: 337–351.
Geng, T., Zheng, F., Kuznetsov, A. V., Roberts, W. L., and Paxson, D. E.. Comparison between numerically simulated and experimentally measured flow field quantities behind a pulsejet. Flow, turbulence and combustion. 2010; 84.4: 653–667.
Akulich, P. V., Kuts, P. S., Samsonyuk, V. K., Severyanin, V. S., and Slizhuk, V. D.. Investigation of a pulsating-combustion chamber. Journal of engineering physics and thermophysics. 2000; 73.3: 477–480.
Yallina, E. V., Larionov, V. M., Iovleva, O. V. Pulsating combustion of gas fuel in the combustion chamber with closed resonant circuit. In: Journal of Physics: Conference Series. IOP Publishing. 2013; p. 012017.
Rafi, Shaik, Kumar, B. Kishore. Design and CFD Analysis of Pulse Jet Engine. 2016.
Avinash, T., Reddy, B. Design and CFD Analysis of Pulse Jet Propulsion Engine. International Journal of Professional Engineering Studies. 2016; 7.
Evans, R. G., Alshami, A. S. Pulse jet orchard heater system development: Part I. Design, construction, and optimization. Transactions of the ASABE. 2009; 52.2: 331–343.
Sayres, John. Computational Fluid Dynamics for Pulsejets and Pulsejet Related Technologies. 2010.
Geng, T., Kiker Jr, A., Ordon, R., Kuznetsov, A.V., Zeng, T.F. and Roberts. Combined numerical and experimental investigation of a hobby-scale pulsejet. Journal of propulsion and power. 2007; 23.1: 186–193.
Schoen, Michael Alexander. Experimental investigations in 15 centimeter class pulsejet engines. 2005.
Ordon, Robert Lewis. Experimental Investigations into the operational parameters of a 50 Centimeter Class Pulsejet Engine. 2006.
Kiker, Adam Paul. Experimental investigations of mini-pulsejet engines. 2005.
Zheng, Fei. Computational Investigation of High-Speed Pulsejets. 2009.
Debnath, Pinku, Pandey, K. M. Numerical investigation of detonation combustion wave propagation in pulse detonation combustor with nozzle. Advances in aircraft and spacecraft science. 2020; 7.3: 187–202.
Guan, Peng, Yanting, A. I. Study on thermal-acoustic-structural performance of Aeroengine Combustor based on Coupled-Field Technology.
Yao, Wei, Ging Wang, Yang Lu. Full-scale Detached Eddy Simulation of kerosene fuelled scramjet combustor based on skeletal mechanism. In: 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. 2015; p. 3579.
Kamal, M. M. NOx emission performance of triple flames. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy. 2007; 221.8: 1193–1208.
Kamal, Mahmoud M. Development of a multiple opposing jets’ burner for premixed flames. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy. 2012; 226.8: 1032–1049.
Kamal, M. M. Development of a cylindrical burner comprising multiple pairs of opposing partially premixed or inverse diffusion flames. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy. 2015; 229.8: 992–1006.
Kamal, M. M. Combustion via multiple pairs of opposing premixed flames with a cross-flow. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy. 2017; 231.1: 39–58.
Yilmaz, Ilker. Effect of swirl number on combustion characteristics in a natural gas diffusion flame. Journal of Energy Resources Technology. 2013; 135.4.
N. Wilkes, P. Guilbert, C. Shepherd, S. Simcox, UKAEA Atomic Energy Research Establishment, H. C. S., Div, S., UKAEA Atomic Energy Research Establishment. E. S. D., The Application of HARWELL-Flow3d to Combustion Problems, UKAEA Atomic Energy Research Establishment Computer Science and Systems Division, 1989.
Chen, Song. Numerical study of a methane jet diffusion flame in a longitudinal tube with a standing wave. Energy Procedia, 2017; 105: 1539–1544.
Fluent, A.N.S.Y.S. Theory Guide 15. Fluent Incorporated. 2013.
Magnussen BF, Hjertager BH. On mathematical modelling of turbulent combustion with special emphasis on soot formation and combustion. In Symposium (international) on Combustion 1977 Jan 1 (Vol. 16, No. 1, pp. 719–729). Elsevier.
Spalart PR, Shur M. On the sensitization of turbulence models to rotation and curvature. Aerospace Science and Technology. 1997 Jul 1;1(5):297–302.
Hosseini AA, Ghodrat M, Moghiman M, Pourhoseini SH. Numerical study of inlet air swirl intensity effect of a Methane-Air Diffusion Flame on its combustion characteristics. Case Studies in Thermal Engineering. 2020 Apr 1;18:100610.
Gray RR, Lindahl TG, Inventors; Hosokawa Micron International Inc 780 Third Avenue New York New York 10017 A Corp of, Sonodyne Industries Inc 11135 SW Capitol HWY Portland or 97219 A Corp of or, Sonodyne Industries Inc A Corp of or, Hosokawa Micron International Inc, assignee. Elevated temperature dehydration section for particle drying pulse jet combustion systems. United States patent US 4,701,126. 1987 Oct 20.
Hamed AM, Moustafa AM, Kamal MM, Hussin AE. Single and Double Flow Pulsations of Normal and Inverse Partially Premixed Methane-Air Flames. Combustion Science and Technology. 2020 Dec 12:1–31.
Guessab A, Aris A, Baki T, Bounif A. The Effects Turbulence Intensity on NOx Formation in Turbulent Diffusion Piloted Flame (Sandia Flame D). Recent Advances in Mechanical Engineering and Mechanics. 2011:144–50.