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International Journal of Aerospace Engineering
Volume 2015, Article ID 312430, 6 pages
http://dx.doi.org/10.1155/2015/312430
Research Article

Solution of Turbine Blade Cascade Flow Using an Improved Panel Method

Department of Aerospace Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

Received 27 September 2015; Revised 19 November 2015; Accepted 22 November 2015

Academic Editor: Linda L. Vahala

Copyright © 2015 Zong-qi Lei and Guo-zhu Liang. 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. L. Hess, “Panel methods in computational fluid dynamics,” Annual Review of Fluid Mechanics, vol. 22, no. 1, pp. 255–274, 1990. View at Publisher · View at Google Scholar · View at Scopus
  2. J. L. Hess and A. M. O. Smith, “Calculation of non-lifting potential flow about arbitrary three-dimensional bodies,” E.S. 40622, Douglas Aircraft Division, 1962. View at Google Scholar
  3. F. A. Woodward, “Analysis and design of Wing-Body combinations at subsonic and supersonic speed,” Journal of Aircraft, vol. 5, no. 6, pp. 528–534, 1968. View at Publisher · View at Google Scholar
  4. L. Morino, “Oscillatory and unsteady subsonic and supersonic aerodynamics—production version (SOUSSA-P.1,1) vol. 1, theoretical manual,” NASA CR-159130, 1980. View at Google Scholar
  5. R. L. Carmichael and L. L. Erickson, “PAN AIR—a higher order panel method for predicting subsonic or supersonic linear potential flows about arbitrary configurations,” in Proceedings of the 14th Fluid and Plasma Dynamics Conference, AIAA Paper 81-1255, Palo Alto, Calif, USA, 1981.
  6. L. Fornasier, “HISS—a higer order subsonic/supersonic singularity method for calculating linearized potential flow,” AIAA Paper 84-1646, 1984. View at Google Scholar
  7. B. Maskew, “Program VSAERO theory document,” NASA CR 4023, 1987. View at Google Scholar
  8. L. Gebhardt, D. Fokin, T. Lutz, and S. Wagner, “An implicit-explicit dirichlet-based field panel method for transonic aircraft design,” in Proceedings of the 20th AIAA Applied Aerodynamics Conference, AIAA 2002-3145, St. Louis, Mo, USA, June 2002.
  9. M. Drela, “XFOIL: an analysis and design system for low reynolds number airfoils,” in Low Reynolds Number Aerodynamics, T. J. Mueller, Ed., vol. 54 of Lecture Notes in Engineering, pp. 1–12, Springer, Berlin, Germany, 1989. View at Publisher · View at Google Scholar
  10. S. Lieblein and N. O. Stockman, “Compressibility correction for internal flow solutions,” Journal of Aircraft, vol. 9, no. 4, pp. 312–313, 1972. View at Publisher · View at Google Scholar
  11. J. L. Hess and A. M. O. Smith, “Calculation of potential flow about arbitrary bodies,” Progress in Aerospace Sciences, vol. 8, pp. 1–138, 1967. View at Publisher · View at Google Scholar · View at Scopus
  12. R. Kiock, F. Lehthaus, N. C. Baines, and C. H. Sieverding, “The transonic flow through a plane turbine cascade as measured in four european wind tunnels,” Journal of Engineering for Gas Turbines and Power, vol. 108, no. 2, pp. 277–284, 1986. View at Publisher · View at Google Scholar · View at Scopus