Table of Contents Author Guidelines Submit a Manuscript
International Journal of Aerospace Engineering
Volume 2013, Article ID 284206, 12 pages
http://dx.doi.org/10.1155/2013/284206
Research Article

Development and Validation of a New Boundary Condition for Intake Analysis with Distortion

Department of Mechanichal Engineering, École Polytechnique de Montréal, 2500, Chemin de Polytechnique, Montréal, QC, Canada H3T 1J4

Received 10 February 2013; Accepted 20 April 2013

Academic Editor: Mark Price

Copyright © 2013 Foad Mehdi Zadeh 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. V. Fidalgo, C. Hall, and Y. Colin, “A study of fan-distortion interaction within the nasa rotor 67 transonic stage,” in ASME Turboexpo Conference, 2010.
  2. H. Pearson and A. McKenzie, “Wakes in axial compressors,” Journal of the Royal Aeronautical Society, vol. 63, pp. 415–416, 1959. View at Google Scholar
  3. C. Reid, “The response of axial flow compressors to intake flow distortion,” in Proceedings of the International Gas Turbine and Aero-Engine Congress and Exhibition, ASME, New York, NY, USA, 1969.
  4. R. S. Mazzawy, “Multiple segment parallel compressor model for circumferential flow distortion(in jet engines),” Journal of Engineering for Power-Transactions of the ASME, vol. 99, no. 2, pp. 288–296, 1977. View at Google Scholar · View at Scopus
  5. A. H. Stenning, “Inlet distortion effects in axial compressors,” Journal of Fluids Engineering, Transactions of the ASME, vol. 102, no. 1, pp. 7–13, 1980. View at Google Scholar · View at Scopus
  6. D. L. Whiteld and A. Jameson, “Three-dimensional Euler equation simulation of propeller-wing interaction in transonic flow,” in Proceedings of the 21st American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting, Reno, Nev, USA, 1983.
  7. T. Q. Dang, “Calculations of propeller/airframe interference effects using the potential/multienergy flow method,” AIAA journal, vol. 28, no. 5, pp. 771–777, 1990. View at Google Scholar · View at Scopus
  8. E. Hsiao, M. Naimi, J. P. Lewis, K. Dalbey, Y. Gong, and C. Tan, “Actuator duct model of turbomachinery components for powered-nacelle Navier-Stokes calculations,” Journal of Propulsion and Power, vol. 17, no. 4, pp. 919–927, 2001. View at Google Scholar · View at Scopus
  9. A. Hale, M. Davis, and J. Sirbaugh, “A numerical simulation capability for analysis of aircraft inlet-engine compatibility,” Journal of Engineering for Gas Turbines and Power, vol. 128, no. 3, pp. 473–481, 2006. View at Publisher · View at Google Scholar · View at Scopus
  10. J. Yao, S. E. Gorrell, and A. R. Wadia, “A time-accurate CFD analysis of inlet distortion induced swirl in multistage fans,” in Proceedings of the 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, pp. 628–641, July 2007. View at Scopus
  11. R. I. Lewis, “Developments of actuator disc theory for compressible flow through turbo-machines,” International Journal of Mechanical Sciences, vol. 37, no. 10, pp. 1051–1066, 1995. View at Google Scholar · View at Scopus
  12. F. Mehdi Zadeh, Amélioration de la Condition Frontière de Face de Soufflante Pour la Conception de L'admission D'Air Sous Distorsion, École Polytechnique de Montréal, 2011.
  13. R. Lewis, Turbomachinery Performance Analysis, vol. 1, Butterworth-Heinemann, 1996.