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International Journal of Aerospace Engineering
Volume 2012 (2012), Article ID 217463, 6 pages
Research Article

Assessment of Combustor Working Environments

Aerospace Research, Gas Turbine Laboratory, The National Research Council of Canada, 1200 Montreal Road, M-10, Ottawa, ON, Canada K1A 0R6

Received 10 March 2012; Accepted 29 June 2012

Academic Editor: Victor Giurgiutiu

Copyright © 2012 Leiyong Jiang and Andrew Corber. 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. J. Bird, M. Mrad, X. Wu, and C. Yang, “Propulsion System Mission and Maintenance Planning Demonstrator,” LTR-GTL-2010-0092, The National Research Council of Canada.
  2. V. L. Oechsle, P. T. Ross, and H. C. Mongia, “High density fuel effects on gas turbine engines,” Tech. Rep. AIAA-87-1829, San Diego, Calif, USA, 1987, AIAA/SAE/ASME/ASEE 23rd Joint Propulsion Conference. View at Google Scholar
  3. P. J. Stuttaford and P. A. Rubini, “Preliminary gas turbine combustor design using a network approach,” Journal of Engineering for Gas Turbines and Power, vol. 119, no. 3, pp. 546–552, 1997. View at Google Scholar · View at Scopus
  4. R. C. Adkins and D. Gueroui, “An improved method for accurate prediction of mass flows through combustor liner holes,” Tech. Rep. GT86-149, Duesseldorf, Germany, 1986. View at Google Scholar
  5. A. H. Lefebvre and D. R. Ballal, Gas Turbine Combustion, Taylor and Francis Group, 2010.
  6. H. C. Mongia, “Recent advances in the development of combustor design tools,” Tech. Rep. AIAA-2003-4495, Huntsville Alabama USA, 2003, AIAA/SAE/ASME/ASEE 39th Joint Propulsion Conference. View at Google Scholar
  7. M. Samimy, K. S. Breuer, L. G. Leal, and P. H. Steen, A Gallery of Fluid Motion, Cambridge University Press, Cambridge, UK, 2003.
  8. L. Y. Jiang and A. Corber, “Benchmark Modeling of T56 Gas Turbine Combustor—phase I, CFD model, flow features, air distribution and combustor can temperature distribution,” LTR-GTL-2010-0088, The National Research Council of Canada, 2011. View at Google Scholar
  9. L. Jiang, “Combustor cooling wiggle strip and geometrical simplification,” in Proceedings of the International Mechanical Engineering Congress and Exposition (IMECE '08), pp. 177–184, November 2008. View at Scopus