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International Journal of Aerospace Engineering
Volume 2016, Article ID 7604279, 14 pages
http://dx.doi.org/10.1155/2016/7604279
Research Article

Parametric Study of Fuel Distribution Effects on a Kerosene-Based Scramjet Combustor

Science and Technology on Scramjet Laboratory, National University of Defense Technology, Changsha, Hunan 410073, China

Received 11 January 2016; Revised 30 May 2016; Accepted 2 June 2016

Academic Editor: James J. McGuirk

Copyright © 2016 Jun Yang et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

Linked References

  1. M. Kodera, S. Tomioka, and T. Kanda, “Mach 6 test of a scramjet engine with boundary-layer bleeding and two-staged fuel injection,” Tech. Rep. NASA/AIAA-2003-7049, NASA, 2003. View at Google Scholar
  2. P. Manna, M. Dharavath, P. K. Sinha, and D. Chakraborty, “Optimization of a flight-worthy scramjet combustor through CFD,” Aerospace Science and Technology, vol. 27, no. 1, pp. 138–146, 2013. View at Publisher · View at Google Scholar · View at Scopus
  3. K. Kumaran and V. Babu, “Mixing and combustion characteristics of kerosene in a model supersonic combustor,” Journal of Propulsion and Power, vol. 25, no. 3, pp. 583–592, 2009. View at Publisher · View at Google Scholar · View at Scopus
  4. X. Y. Wu, X. S. Li, M. Ding, W. D. Liu, and Z. G. Wang, “Experimental study on effects of fuel injection on scramjet combustor performance,” Chinese Journal of Aeronautics, vol. 20, no. 6, pp. 488–494, 2007. View at Publisher · View at Google Scholar · View at Scopus
  5. G. Yu, J. G. Li, X. Y. Chang, L. H. Chen, and C. J. Sung, “Investigation of kerosene combustion characteristics with pilot hydrogen in model supersonic combustors,” Journal of Propulsion and Power, vol. 17, no. 6, pp. 1263–1272, 2001. View at Publisher · View at Google Scholar · View at Scopus
  6. X. Fan, G. Yu, J. Li, X. Zhang, and C.-J. Sung, “Investigation of vaporized kerosene injection and combustion in a supersonic model combustor,” Journal of Propulsion and Power, vol. 22, no. 1, pp. 103–110, 2006. View at Publisher · View at Google Scholar · View at Scopus
  7. M. Ali and A. K. M. S. Islam, “Study on main flow and fuel injector configurations for Scramjet applications,” International Journal of Heat and Mass Transfer, vol. 49, no. 19-20, pp. 3634–3644, 2006. View at Publisher · View at Google Scholar · View at Zentralblatt MATH · View at Scopus
  8. N. Wang, J. Zhou, Y. Pan, and H. Wang, “Experimental investigation on flow patterns of RP-3 kerosene under sub-critical and supercritical pressures,” Acta Astronautica, vol. 94, no. 2, pp. 834–842, 2014. View at Publisher · View at Google Scholar · View at Scopus
  9. K. Kumaran, P. R. Behera, and V. Babu, “Numerical investigation of the supersonic combustion of kerosene in a strut-based combustor,” Journal of Propulsion and Power, vol. 26, no. 5, pp. 1084–1091, 2010. View at Publisher · View at Google Scholar · View at Scopus
  10. K. Deb, A. Pratap, S. Agarwal, and T. Meyarivan, “A fast and elitist multiobjective genetic algorithm: NSGA-II,” IEEE Transactions on Evolutionary Computation, vol. 6, no. 2, pp. 182–197, 2002. View at Publisher · View at Google Scholar · View at Scopus
  11. G. Choubey and K. M. Pandey, “Effect of variation of angle of attack on the performance of two-strut scramjet combustor,” International Journal of Hydrogen Energy, vol. 41, no. 26, pp. 11455–11470, 2016. View at Publisher · View at Google Scholar
  12. H. B. Ebrahimi, D. V. Gaitonde, and F. J. Malo-Molina, “Parametric study of 3-D hydrocarbon scramjet engine with cavity,” in Proceedings of the 45th AIAA Aerospace Sciences Meeting and Exhibit, AIAA 2007-645, pp. 7773–7787, Reno, Nev, USA, January 2007. View at Scopus
  13. K. M. Pandey and Sivasakthivel, “CFD analysis of mixing and combustion of a scramjet combustor with a planer strut injector,” International of Environmental Science and Development, vol. 2, no. 2, pp. 102–108, 2011. View at Google Scholar
  14. Y. You, H. Luedeke, and K. Hannemann, “Injection and mixing in a scramjet combustor: DES and RANS studies,” Proceedings of the Combustion Institute, vol. 34, no. 2, pp. 2083–2092, 2013. View at Publisher · View at Google Scholar · View at Scopus
  15. A. Mangeot, N. Gascoin, and P. Gillard, “Methodologies for detailed chemistry computation application to hybrid rocket combustion chamber simulations,” in Proceedings of the 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, AIAA, San Jose, Calif, USA, 2013. View at Publisher · View at Google Scholar
  16. K. Park, P.-K. Oh, and H.-J. Lim, “The application of the CFD and Kriging method to an optimization of heat sink,” International Journal of Heat and Mass Transfer, vol. 49, no. 19-20, pp. 3439–3447, 2006. View at Publisher · View at Google Scholar · View at Scopus
  17. P. Dagaut, A. El Bakali, and A. Ristori, “The combustion of kerosene: experimental results and kinetic modelling using 1- to 3-component surrogate model fuels,” Fuel, vol. 85, no. 7-8, pp. 944–956, 2006. View at Publisher · View at Google Scholar · View at Scopus
  18. P. Dagaut, F. Karsenty, G. Dayma et al., “Experimental and detailed kinetic model for the oxidation of a Gas to Liquid (GtL) jet fuel,” Combustion and Flame, vol. 161, no. 3, pp. 835–847, 2014. View at Publisher · View at Google Scholar · View at Scopus
  19. S. Honnet, K. Seshadri, U. Niemann, and N. Peters, “A surrogate fuel for kerosene,” Proceedings of the Combustion Institute, vol. 32, pp. 485–492, 2009. View at Publisher · View at Google Scholar · View at Scopus
  20. P. Dagaut and M. Cathonnet, “The ignition, oxidation, and combustion of kerosene: a review of experimental and kinetic modeling,” Progress in Energy and Combustion Science, vol. 32, no. 1, pp. 48–92, 2006. View at Publisher · View at Google Scholar · View at Scopus
  21. M. Zhang, Z. Zhu, G. He, and P. Liu, “Large-eddy simulation of kerosene spray combustion in a model scramjet chamber,” Proceedings of the IMechE Part G: Journal of Aerospace Engineering, vol. 224, no. 9, pp. 949–960, 2010. View at Google Scholar
  22. T. S. Wang, “Thermophysics characterization of kerosene combustion,” Journal of Thermophysics and Heat Transfer, vol. 15, no. 2, pp. 140–147, 2001. View at Publisher · View at Google Scholar
  23. D. J. Hautman, F. L. Dryer, K. P. Schug, and I. Glassman, “A multi-step overall kinetic mechanism for the oxidation of hydrocarbons,” Combustion Science and Technology, vol. 25, no. 5, pp. 219–235, 1981. View at Publisher · View at Google Scholar
  24. G. Y. Gerasimov and S. A. Losev, “Kinetic models of combustion of kerosene and its components,” Journal of Engineering Physics and Thermophysics, vol. 78, no. 6, pp. 1059–1070, 2005. View at Publisher · View at Google Scholar · View at Scopus
  25. S. K. Srlvatsa, “Computations of soot and NOX emissions from gas turbine combustors,” NASA CR-167930, 1982. View at Google Scholar
  26. J.-S. Park, “Optimal Latin-hypercube designs for computer experiments,” Journal of Statistical Planning and Inference, vol. 39, no. 1, pp. 95–111, 1994. View at Publisher · View at Google Scholar · View at Zentralblatt MATH · View at MathSciNet · View at Scopus
  27. J. Yim, B. J. Lee, and C. Kim, “Exploring multi-stage shape optimization strategy of multi-body geometries using Kriging-based model and adjoint method,” Computers & Fluids, vol. 68, pp. 71–87, 2012. View at Publisher · View at Google Scholar · View at Scopus
  28. F. Boukouvala and M. G. Ierapetritou, “Feasibility analysis of black-box processes using an adaptive sampling Kriging-based method,” Computers & Chemical Engineering, vol. 36, no. 1, pp. 358–368, 2012. View at Publisher · View at Google Scholar · View at Scopus
  29. R. A. Baurle, T. Mathur, M. R. Gruber, and K. R. Jackson, “A numerical and experimental investigation of a scramjet combustor for hypersonic missile applications,” AIAA Paper 98-3121, 1998. View at Google Scholar
  30. iSIGHT software, http://www.simulia.com.