45.10. References

The following reference works were consulted when creating this example problem:

  1. Lim, S.H., Bladh, R., Castanier, M. P., & Pierre, C. (2007). Compact, generalized component mode mistuning representation for modeling bladed disk vibration. AIAA Journal. 45.9: 2285-2298.

  2. Singh, M.P., Vargo, J. J., Schiffer, D. M., & Dello, J. D. (1988). SAFE diagram: A design and reliability tool for turbine blading. 17th Turbomachinery Symposium. Dallas, TX.

  3. Castanier, M.P. & Pierre, C. (2006). Modeling and Analysis of Mistuned Bladed Disk Vibration: Status and Emerging Directions. Journal of Propulsion and Power. 22.2.

  4. Rzadkowski, R., Drewczynski, M., Maurin, M., & Szczepanik, R. (2011). Forced response of the mistuned first stage compressor bladed disc of an aircraft engine - Experimental and numerical results. 13th World Congress in Mechanism and Machine Space. Guanajuato, Mexico.

  5. Elder, R., Patil, S., Homes, W. (2013). Investigation of Efficient CFD Methods for the Prediction of Blade Damping. Proceedings of ASME Turbo Expo 2013. San Antonio, TX.

  6. Zhang, C., Ye, Z., Liu, F. (2009). Numerical researches on aeroelastic problem of a rotor due to IGV/fan interaction. AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition.Orlando, FL.