Abstract
Regenerative cooling with fuel as the coolant is used in the scramjet engine. In order to grasp the dynamic characteristics of engine fuel supply processes, this article studies the dynamic characteristics of hydrocarbon fuel within the channel. A one-dimensional dynamic model was proved, the thermal energy storage effect, fuel volume effect and chemical dynamic effect have been considered in the model, the ordinary differential equations were solved using a 4th order Runge-Kutta method. The precision of the model was validated by three groups of experimental data. The effects of input signal, working condition, tube size on the dynamic characteristics of pressure, flow rate, temperature have been simulated. It is found that cracking reaction increased the compressibility of the fuel pyrolysis mixture and lead to longer responding time of outlet flow. The responding time of outlet flow can reach 3s when tube is 5m long which will greatly influence the control performance of the engine thrust system. Meanwhile, when the inlet flow rate appears the step change, the inlet pressure leads to overshoot, the overshoot can reach as much as 100%, such highly transient impulse will result in detrimental effect on fuel pump.
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References
E.T. Curran, “Scramjet engines: the first forty years”, J Propulsion Power, 17 (6) (2001), pp. 1138–1148.
Hopkins R.P., Raymond N.E., White S.T., DeLong S., “The Analysis of Conventional Prompt Global Strike Alternatives”, 2010 IEEE Systems and Information Engineering Design Symposium, Charlottesville, Virginia, USA, 2010: 135–140.
Richman M.S., Kenyon J.A., “High Speed and Hypersonic Science and Technology”, 41st AIAA/ASME/ASEE Joint Propulsion Conference and Exhibit, Tucson, Arizona, AIAA 2005-4099, 2005.
Smart M.K., Hass N.E., and Paull A., “Flight Data Analysis of the HyShot 2 Scramjet Flight Experiment”, AIAA Journal, Vol. 44, No. 10, 2006, pp. 2366–2375.
J.T. Chang, W. Bao, D.R. Yu., “Hypersonic inlet control with pulse periodic energy addition”, Proc IMechE Part G J Aerospace Eng, 223 (2009), pp. 85–94.
Jiang Qin, Wen Bao, Silong Zhang, and Weixing Zhou., “Comparison During a Scramjet Regenerative Cooling and Recooling Cycle”, Journal of Thermophysics and Heat Transfer, Vol. 26, No. 4 (2012), pp. 612–618.
Silong Zhang, Yu Feng, Yuguang Jiang, “Thermal behavior in the cracking reaction zone of scramjet cooling channels at different channel aspect ratios”, Acta Astronautica, Volume 127, October–November 2016, Pages 41–56.
Oberkampf W. L., Trucano T. G., “Verification and Validation in Computational Fluid Dynamics”, Progress in Aerospace Sciences, Vol. 38, No. 3, April 2002, pp. 209–272.
T.A. Ward, J.S. Ervin, S. Zabarnick, L. Shafer, “Pressure effects on flowing mildly-cracked n-Decane”, J. Propuls. Power, 21 (2) (2005), pp. 344–355
Silong Zhang, Yu Feng, Yuguang Jiang, “Thermal behavior in the cracking reaction zone of scramjet cooling channels at different channel aspect ratios”, Acta Astronautica, Volume 127, October–November 2016, Pages 41–56.
T.A. Ward, J.S. Ervin, R.C. Striebich, S. Zabarnick, “Simulations of flowing mildly-cracked normal alkanes incorporating proportional product distributions”, J. Propuls. Power, 20 (3) (2004), pp. 394–402
Linne D.L., Meyer M.L., Braun D.C., et al, “Investigation of Instabilities and Heat Transfer Phenomena in Supercritical Fuels at High Heat Flux and Temperatures”, 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit Las Vegas, Nevada, U.S.A. AIAA 2000-3128, 2000.
Nicolas Gascoin, Philippe Gillard, Emmanuel Dufour, and Youssoufi Touré. “Validation of Transient Cooling Modeling for Hypersonic Application”, Journal of Thermophysics and Heat Transfer, Vol. 21, No. 1 (2007), pp. 86–94.
Dahm K.D., Virk P.S., Bounaceur R., Battin-Leclerc F., Marquaire P.M., Fournet R., Daniau E., and Bouchez M., “Experimental and Modeling Investigation of the Thermal Decomposition of n-Dodecane”, Journal of Analytical and Applied Pyrolysis, Vol. 71, No. 2, June 2004, pp. 865–881.
W Bao, X-L Li, J Qin, and W-X Zhou, “Modeling and simulation methodology of channel cooling using hydrocarbon fuel as coolant under supercritical pressures”, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. Vol 225 Issue 9, pp. 969–984.
T.A. Ward, J.S. Ervin, R.C. Striebich, S. Zabarnick, “Simulations of flowing mildly-cracked normal alkanes incorporating proportional product distributions”, J. Propuls. Power, 20 (3) (2004), pp. 394–402.
J. Stewart, K. Brezinsky, I. Glassman, “Supercritical pyrolysis of Decalin, Tetralin, and n–Decane at 700–800 K. Product distribution and reaction mechanism”, Combust. Sci. Technol., 136 (1998), pp. 373–390.
D.Y. Peng, D.B. Robinsion, “A new two-constant equation of state Ind. Eng. Chem. Fundam”, 51 (1) (1976), pp. 59–64.
E. Bruce Poling, J.M. Prausnitz, O.J. Paul, “The Properties of Gases and Liquids”, 5, McGraw-Hill, New York (2001).
E.W. Lemmon, L.H. Marcia, M.O. Mclinden, “NIST 23: Reference Fluid Thermodynamic and Transport Properties”, NIST Standard Reference Database Number 23, Version 9.1. NIST, 2013.
W. Bao, S. Zhang, J. Qin, W. Zhou, K. Xie. “Numerical analysis of flowing cracked hydrocarbon fuel inside cooling channels in view of thermal management”, Energy, 67 (2014), pp. 149–161
ANSYS FLUENT User's Guide, Release 13.0, November 2010.
O. Redlich, J.N.S. Kwong On the thermodynamics of solutions. V. “An equation of state”, Fugacities of gaseous solutions Chem. Rev., 44 (1) (1949), pp. 233–244.
Z. Jia, H. Huang, W. Zhou, et al. Experimental and modeling investigation of n-Decane pyrolysis at supercritical pressures, Energy Fuels, 28 (9) (2014), pp. 6019–6028.
W. Zhou, Z. Jia, J. Qin, et al. Experimental study on effect of pressure on heat sink of n-Decane, Chem. Eng. J., 243 (2014), pp. 127–136
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Yu, B., Zhou, W., Qin, J. et al. Dynamic characteristics of hydrocarbon fuel within the channel at supercritical and pyrolysis condition. J. Therm. Sci. 26, 560–569 (2017). https://doi.org/10.1007/s11630-017-0974-z
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DOI: https://doi.org/10.1007/s11630-017-0974-z