Table of Contents Author Guidelines Submit a Manuscript
International Journal of Rotating Machinery
Volume 2015 (2015), Article ID 198534, 10 pages
Research Article

Detection of Rotor Forced Response Vibrations Using Stationary Pressure Transducers in a Multistage Axial Compressor

Purdue University, 500 Allison Road, West Lafayette, IN 47907, USA

Received 23 July 2014; Revised 31 October 2014; Accepted 3 November 2014

Academic Editor: Mark McQuilling

Copyright © 2015 William L. Murray III and Nicole L. Key. 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. O. Freund, M. Bartelt, M. Mittelbach, M. Montgomery, D. M. Vogt, and J. R. Seume, “Impact of the flow on an acoustic excitation system for Aeroelastic studies,” ASME Journal of Turbomachinery, vol. 135, no. 3, Article ID 031033, 2013. View at Publisher · View at Google Scholar · View at Scopus
  2. M. Baumgartner, F. Kameier, and J. Hourmouzaiadis, “Non-engine order blade vibration in a high pressure compressor,” in Proceedings of the ISABE International Symposium on Airbreathing Engines, Melbourne, Australia, September 1995.
  3. J. D. Gill and V. R. Capece, “Experimental investigation of flutter in a single stage unshrouded axial-flow fan,” in Proceedings of the 42nd AIAA Aerospace Sciences Meeting and Exhibit, pp. 7997–8005, Reno, Nev, USA, January 2004. View at Scopus
  4. V. Mengle, “Acoustic spectra and detection of vibrating rotor blades, including row-to-row interference,” in Proceedings of the AIAA 13th Aeroacoustics Conference, Tallahassee, Fla, USA, October 1990.
  5. A. P. Kurkov, “Flutter spectral measurements using stationary pressure transducers,” Journal of Engineering for Power, vol. 103, no. 2, pp. 461–467, 1981. View at Publisher · View at Google Scholar · View at Scopus
  6. S. Leichtfuss, F. Holzinger, C. Brandstetter, F. Wartzek, and H. P. Schiffer, “Aeroelastic investigation of a transonic research compressor,” in Proceedings of ASME Turbo Expo, San Antonio , Tex, USA, June 2013.
  7. H. Schoenenborn and T. Breuer, “Aeroelasticity at reversed flow conditions—part II: application to compressor surge,” Journal of Turbomachinery, vol. 134, no. 6, Article ID 061031, 8 pages, 2012. View at Publisher · View at Google Scholar
  8. J. Fridh, B. Laumert, and T. Fransson, “Forced response in axial turbines under the influence of partial admission,” Journal of Turbomachinery, vol. 135, no. 3, Article ID 041014, pp. 041014-1–041014-9, 2013. View at Publisher · View at Google Scholar · View at Scopus
  9. R. D. Fulayter, An experimental investigation of resonant response of mistuned fan and compressor rotors utilizing NSMS [Ph.D. dissertation], School of Mechanical Engineering, Purdue University, West Lafayette, Ind, USA, 2004.
  10. A. von Flotow, Hood Technologies Corporation’s Analyze Blade Vibration Software Version 3.3 User Manual, 2003.
  11. D. S. Whitehead, “Unsteady two-dimensional linearized subsonic flow in cascades,” in AGARD Manual on Aeroelasticity in Axial-Flow Turbomachines, vol. 1, pp. 3.24–3.30, 1987. View at Google Scholar