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International Journal of Rotating Machinery
Volume 2011, Article ID 182906, 8 pages
Research Article

Development of a Method for Enhanced Fan Representation in Gas Turbine Modeling

1Department of Power and Propulsion, SOE, Cranfield University, Bedfordshire MK43 0AL, UK
2Department of Mechanical Engineering, Aristotle University of Thessaloniki, 54124 Thessaloniki, Greece

Received 1 November 2010; Revised 11 May 2011; Accepted 17 May 2011

Academic Editor: M. Razi Nalim

Copyright © 2011 Georgios Doulgeris 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. P. Walsh and P. Fletcher, Gas Turbine Performance, Blackwell, 2nd edition, 2004.
  2. H. I. H. Saravanamuttoo, G. F. C. Rogers, and H. Cohen, Gas Turbine Theory, Pearson Education, 5th edition, 2001.
  3. J. D. Mattingly, W. H. Heiser, and D. T. Pratt, Aircraft Engine Design, AIAA Education Series, Reston, Va, USA, 2nd edition, 2002.
  4. S. Lieblien, “Characteristics of two-dimensional compressor blade cascades,” NACA-RM-E 57A28, Washington, DC, USA, 1957. View at Google Scholar
  5. G. A. Plourde, A. H. Stenning, U. Lehigh, and P. Bethlehem, “Attenuation of circumferential inlet distortion in multistage axial compressors,” Journal of Aircraft, vol. 5, pp. 236–242, 1968. View at Google Scholar
  6. G. M. Callahan and A. H. Stenning, “Attenuation of inlet flow distortion upstream of axial flow compressors,” in Proceedings of the AIAA 5th Propulsion Joint Specialist Conference, Colo, USA, 1969.
  7. H. Pearson and A. B. McKenzie, “Wakes in axial compressors,” Journal of the Royal Aeronautical Society, pp. 415–416, 1959. View at Google Scholar
  8. C. Reid, “The response of axial flow compressor to intake flow distortion,” ASME 69-GT-29, 1969. View at Google Scholar
  9. J. E. Calogeras, C. M. Mehalic, and P. L. Burstadt, “Experimental investigation of the effect of screen-induced total-pressure distortion on turbojet stall margin,” NASA-TM-X 2239, 1971. View at Google Scholar
  10. E. J. Milner and L. M. Wenzel, “Performance of a J85-13 compressor with clean and distorted inlet flow,” NASA-TM-X 3304, 1975. View at Google Scholar
  11. W. M. Braithwaite, E. J. Graber, and C. M. Mehalic, “The effect of inlet temperature and pressure distortion on turbojet performance,” AIAA 73-1316, 1973. View at Google Scholar
  12. E. M. Greitzer and H. R. Griswold, “Compressor-diffuser interaction with circumferential flow distortion,” Journal Mechanical Engineering Science, vol. 18, no. 1, pp. 25–38, 1976. View at Google Scholar
  13. L. M. Wenzel and R. J. Blaha, “Analysis of dynamic inlet distortion applied to a parallel compressor model,” NASA-TM-X 3522, 1977. View at Google Scholar
  14. R. S. Mazzawy, “Multiple segment parallel compressor model for circumferential flow distortion,” Journal of Engineering for Power. Transactions of the ASME, vol. 99, no. 2, pp. 288–296, 1977. View at Google Scholar · View at Scopus
  15. A. Elder, “Prediction of the effect of distorted inlet flows on fan and compressor stability,” IMechE C117/84, 1984. View at Google Scholar
  16. J. Yin and P. Pilidis, “Influence of inlet profile on high-BPR turbofan performance using a radial profile map,” in Proceedings of the ICAS Congress, 2002.
  17. J. Yin, R. Hales, P. Pilidis, and B. Curnock, “2-shaft high-bypass ratio turbofan performance calculation using a new 2-D fan model,” in Proceedings of the 37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Salt Lake City, Utah, USA, July 2001.
  18. V. Pachidis, P. Pilidis, I. Templalexis, T. Korakianitis, and P. Kotsiopoulos, “Prediction of engine performance under compressor inlet flow distortion using streamline curvature,” Journal of Engineering for Gas Turbines and Power, vol. 129, no. 1, pp. 97–103, 2007. View at Publisher · View at Google Scholar · View at Scopus
  19. V. Pachidis, P. Pilidis, F. Talhouarn, A. Kalfas, and I. Templalexis, “A fully integrated approach to component zooming using computational fluid dynamics,” Journal of Engineering for Gas Turbines and Power, vol. 128, no. 3, pp. 579–584, 2006. View at Publisher · View at Google Scholar · View at Scopus
  20. N. L. Sanger, “Performance of a 1.57-pressure-ratio transonic fan stage with a screen-induced 90o circumferential inlet flow distortion,” NASA-TN-D 8163, 1976. View at Google Scholar
  21. N. A. Cumpsty, Compressor Aerodynamics, Longman Scientific & Technical, Longman Group, UK, 1989.
  22. J. Seddon and E. L. Goldsmith, Intake Aerodynamics, Collins, London, UK, 1985.
  23. J. P. Longley and E. M. Greitzer, Steady and Transient Performance Prediction of Gas Turbine Engines, AGARD Lecture Series 183, Inlet Distortion Effects in Aircraft Propulsion System Integration, 1992.
  24. V. Pachidis, Gas turbine advanced performance simulation, Ph.D. thesis, Cranfield University, UK, 2006.
  25. I. Templalexis, Turbine performance with distorted inlet flow, Ph.D. thesis, Cranfield University, UK, 2006.
  26. W. C. Swan, “A practical method of predicting transonic-compressor performance,” Journal of Engineering for Power, vol. 86, pp. 322–330, 1961. View at Google Scholar
  27. H. R. Griepentrog, “Secondary flow losses in axial compressors,” AGARD Lecture Series, no. 39, 1970. View at Google Scholar
  28. D. C. Urasek, W. T. Gorrell, and W. S. Cunnan, “Performance of two-stage fan having low-aspect-ratio, first-stage rotor blading,” Technical Report 78-49 NASA-TP-1493, 1979. View at Google Scholar
  29. J. F. Schmidt and R. S. Ruggeri, “Performance with and without inlet radial distortion of a transonic fan stage designed for reduced loading in the tip region,” NASA-TP 1294, 1978. View at Google Scholar