1. (1) Hsiao-Wei, D. Chang and E. Kielb, 1992, “An Analysis System for Blade Forced Response”, ASME Paper 92-GT-172.
2. (2) D. Kato, I. Mizuta, T. Watase, H. Hattori and K. Kobayashi, 1999, “Prediction of High-Order-Mode Blade Forced Response in a Transonic Axial Compressor”, 14th International Symposium on Air-Breathing Engines, Italy, ISABE-99-7031.
3. (3) K. Nakano, H. Hattori, and Y. Hirata, 2003, “Study on Blade Forced Vibration Response of Radial Inflow Turbine”, Proc. 8th International Gas Turbine Congress Gas Turbine Society of Japan, Tokyo, TS-053.
4. (4) S. T. Kitson et al, 2006, “Improving analysis capability in order to reduce turbine HCF”, Proc. Turbochargers and turbocharging, 8th international conference, London, 17-18 May 2006, p261-271
5. (5) T. Yokoyama, Y. Hayashi, K. Osako, and Y. Komatsu, “Numerical and Experimental Study of Turbine Blade Vibration in Variable Geometry Turbochargers”, SAE International, 2005-01-1855