Numerical calculation of rotating detonation chamber
Abstract
ANSYS FLUENT 14 supplied the CFD tools used in the numerical calculation of rotating detonation combustion. Duringcalculations, various fuel injection methods and configurations of combustion chamber were applied in an attempt to obtainstable and correct detonation propagation results in a separated fuel-air injection system (non-premixed combustion model).However, FLUENT was not originally designed for detonation combustion and the failure to achieve re-initiation of detonationafter collision was always the core issue in the non-premixed combustion model. Thus, this paper mainly focuses on researchinto the behavior of stable continuously rotating detonation in premixed combustion cases. The analysis of stable continuouslyrotating detonation behaviors and structures was carried out with different boundary conditions and mesh cells. Thepressures were measured by using a number of artificial sensors inserted near the chamber outside surface in various axialand/or circumferential directions. With those key results in the case of premixed combustion, we were able to comparably concludethat stable rotating detonation would also be generated if the refilling process were properly exhibited in non-premixedcombustion. The paper finishes with evaluations and conclusions regarding general detonation behaviors and performances.References
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47 (284) (1899) 90–104.
[2] E. Jouguet, Sur la propagation des réactions chimiques dans les gaz,
J. Math. Pures Appl 1 (1905) 347–425.
[3] B. V. Voitsekhovskii, V. V. Mitrofanov, M. E. Topchiyan, Structure of the
detonation front in gases, Izdatielstvo SO AN SSSR.
[4] J. A. Nicholls, H. R. Wilkinson, R. B. Morrison, Intermittent detonation
as a thrust-producing mechanism, Journal of jet propulsion 27 (5)
(1957) 534–541.
[5] A. Tobita, T. Fujiwara, P. Wolanski, Detonation engine and flying object
provided therewith, uS Patent 7,784,267 (Aug. 31 2010).
[6] F. A. Bykovskii, V. V. Mitrofanov, E. F. Vedernikov, Continuous detonation
combustion of fuel-air mixtures, Combustion, Explosion and Shock
Waves 33 (3) (1997) 344–353.
[7] F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov, Continuous spin detonation
in annular combustors, Combustion, Explosion, and Shock Waves
41 (4) (2005) 449–459.
[8] F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov, Continuous spin detonation
of hydrogen-oxygen mixtures. 1. annular cylindrical combustors,
Combustion, Explosion, and Shock Waves 44 (2) (2008) 150–162.
[9] F. A. Bykovskii, E. F. Vedernikov, Continuous detonation of a subsonic
flow of a propellant, Combustion, Explosion, and Shock Waves 39 (3)
(2003) 323–334.
[10] P. Wolanski, J. Kindracki, T. Fujiwara, An experimental study of small
rotating detonation engine, Pulsed and continuous detonations (2006)
332–338.
[11] J. Kindracki, P. Wolanski, Z. Gut, Experimental research on the rotating
detonation in gaseous fuels–oxygen mixtures, Shock waves 21 (2)
(2011) 75–84.
[12] M. Hishida, T. Fujiwara, P. Wolanski, Fundamentals of rotating detonations,
Shock waves 19 (1) (2009) 1–10.
[13] T. Yamada, K. Hayashi, N. Tsuboi, E. Yamada, V. Tangirala, T. Fujiwara,
Numerical analysis of threshold of limit detonation in rotating
detonation engine, in: 48th AIAA Aerospace Sciences Meeting Including
the New Horizons Forum and Aerospace Exposition, 2010, p. 153.
[14] S. Liu, Z. Lin, W.-D. Liu, W. Lin, Research on continuous rotating detonation
wave propagation process (ii): Two-wave collision propagation
mode, Tuijin Jishu/Journal of Propulsion Technology 35 (2) (2014)
269–275.
[15] R. Zhou, J.-P. Wang, Numerical investigation of flow particle paths and
thermodynamic performance of continuously rotating detonation engines,
Combustion and Flame 159 (12) (2012) 3632–3645.
[16] F. Falempin, E. Daniau, N. Getin, F. Bykovskii, S. Zhdan, Toward
a continuous detonation wave rocket engine demonstrator, in: 14th
AIAA/AHI Space Planes and Hypersonic Systems and Technologies
Conference, 2006, p. 7956.
[17] V. Mikhailov, M. Topchiyan, Studies of continuous detonation in an annular
channel, Fizika Goreniya I Vzryva 1 (4) (1965) 20–23.
[18] D. Schwer, K. Kailasanath, Numerical study of the effects of engine
size n rotating detonation engines, in: 49th AIAA Aerospace Sciences
Meeting including the New Horizons Forum and Aerospace Exposition,
2011, p. 581.
[19] S. A. Zhdan, A. M. Mardashev, V. V. Mitrofanov, Calculation of the flow
of spin detonation in an annular chamber, Combustion, Explosion, and
Shock Waves 26 (2) (1990) 210–214.
[20] C. Nordeen, D. Schwer, F. Schauer, J. Hoke, B. Cetegen, T. Barber,
Thermodynamic Modeling of a Rotating Detonation Engine, in:
49th AIAA Aerospace Sciences Meeting including the New Horizons
Forum and Aerospace Exposition, Aerospace Sciences Meetings,
American Institute of Aeronautics and Astronautics, 2011.
doi:doi:10.2514/6.2011-803.
URL http://dx.doi.org/10.2514/6.2011-803
[21] M. Folusiak, A. Kobiera, P. Wolanski, Rotating detonation engine simulations
in-house code-reflops, Prace Instytutu Lotnictwa (2010) 3–23.
[22] J. Wang, Research progress on crde at peking university, Tech. rep.,
Center for Combustion and Propulsion. Peking University (2009).
[23] J. Kindracki, Badania eksperymentalne i symulacje numeryczne procesu
wiruja˛cej detonacji gazowej, Ph.D. thesis, Warsaw University of
Technology (2008).
Published
2018-01-23
How to Cite
KINDRACKI, Jan; SHI, Zhenda.
Numerical calculation of rotating detonation chamber.
Journal of Power Technologies, [S.l.], v. 97, n. 4, p. 314–326, jan. 2018.
ISSN 2083-4195.
Available at: <https://papers.itc.pw.edu.pl/index.php/JPT/article/view/944>. Date accessed: 27 dec. 2024.
Issue
Section
Combustion and Fuel Processing
Keywords
Rotating detonation engine, premixed/non-premixed combustion, 2D/3D chamber model
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