Cite

[1] Beretta-Müller, A. & Szwedowicz, J. (2015). Blade Resonant Forced Response Excited by Combustor Acoustic Eigenmodes. In: Proceedings of ASME Turbo Expo: Turbine Technical Conference and Exposition, June 15 19, 2015, Montreal, Quebec, Canada. Search in Google Scholar

[2] Corral, R. (2012). Bladed Disks: Flutter, Structural Design of Aircraft Engines, RTOAVT-207-06, 25 January, Belgium. Search in Google Scholar

[3] Dodds, J., and Vahdati, M. (May 1, 2015). Rotating Stall Observations in a High Speed Compressor—Part II: Numerical Study. ASME. J. Turbomach. May 2015, Vol. 137, No. 5, 051003. DOI: 10.1115/1.4028558. Open DOISearch in Google Scholar

[4] El-Aini, Y., et al. (1997). High Cycle Fatigue of Turbomachinery Components-Industry Perspective, In: 33rd Joint Propulsion Conference. DOI: 10.2514/6.1997-3365. Open DOISearch in Google Scholar

[5] Han, Y., Xiao, B. & Mignolet, M. P. (2007). Expedient Estimation of the Maximum Amplification Factor in Damped Mistuned Bladed Disks, ASME Paper No. GT2007-27353, In: Proceedings of ASME Turbo Expo, May 14 15, 2007, Montreal, Canada. Search in Google Scholar

[6] Hulme, J. C., Fiebiger, W., S. & Szwedowicz, J. (2015). Axial Compressor Blade Failure Design Mitigation and Its Validation, ASME Paper No. GT2015-43312, ISBN: 978-0-7918-5679-6, Proceedings of ASME Turbo Expo, June 15 19, 2015, Montreal, Canada. Search in Google Scholar

[7] Kenyon, J.A, & Griffin, J.H. (2001). Forced Response of Turbine Engine Bladed Disks and Sensitivity to Harmonic Mistuning. In: Proceedings of the ASME Turbo Expo: Power for Land, Sea, and Air. Volume 4: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; IGTI Scholar Award. New Orleans, Louisiana, USA. June 4–7, 2001. V004T03A037. ASME. DOI: 10.1115/2001-GT-0274. Open DOISearch in Google Scholar

[8] Kurnik, W. (1997). Bifurkacje dywergentne i oscylacyjne, WNT, Warszawa, ISBN 83-204-2221-3. Search in Google Scholar

[9] Moneta, G. (2019). Damping Optimization of Turbine Blade Vibration, Ph.D. Dissertation, Warsaw University of Technology. Search in Google Scholar

[10] Moneta, G. & Jachimowicz, J. (2020). Impact of Manufacturing Tolerances on Stress in a Turbine Blade Fir-Tree Root, Fatigue of Aircraft Structures, Vol. 2020, No. 12, 92 101, DOI: 10.2478/fas-2020-0009. Open DOISearch in Google Scholar

[11] Moneta, G., Jachimowicz, J. & Osiński, J. (2014). Influence of Manufacturing Tolerances on Vibration Frequencies of Turbine Blade, Machine Dynamics Research, Vol. 38, No 1, 105 118. Search in Google Scholar

[12] Peter, J. (1999). The History of Aircraft Gas Turbine Engine Development in the United States: A Tradition of Excellence, ASME IGTI publication. Search in Google Scholar

[13] Schneider C.M., et. al. (2013). On the Unsteady Formation of Secondary Flow Inside a Rotating Turbine Blade Passage. ASME. J. Turbomach., Vol. 136, No. 6, 061004-061004-10. DOI:10.1115/1.4025582. Open DOISearch in Google Scholar

[14] Srinivasan, A.V. (1997). Flutter and Resonant Vibration Characteristics of Engine Blades. In: Proceedings of the ASME International Gas Turbine and Aeroengine Congress and Exhibition. Volume 4: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; IGTI Scholar Award. Orlando, Florida, USA. June 2–5, 1997. V004T17A001. ASME. DOI: 10.1115/97-GT-533. Open DOISearch in Google Scholar

[15] Szwedowicz, J. (2008). High Cyclic Fatigue, Structural Design of Aircraft Engines: Key Objectives & Techniques. Lecture Series Monographs of von Karman Institute for Fluid Dynamics, B-1640 Rhode Saint Genèse, Belgium, ISSN: 0377-8312, ISBN: 978-2-930389-8-2-6, pp. 49. Search in Google Scholar

[16] Szwedowicz, J. (2010, April). 30-year anniversary of friction damper technology in turbine blades. Mechanical Engineering-CIME, Vol. 132, No. 4, 54+. https://link.gale.com/apps/doc/A223657423/AONE?u=googlescholar&sid=bookmark-AONE&xid=d990d10d.10.1115/1.2010-Apr-8 Search in Google Scholar

[17] Szwedowicz, J., et al. (April 3, 2008). Scaling Concept for Axial Turbine Stages With Loosely Assembled Friction Bolts: The Linear Dynamic Assessment. ASME. J. Eng. Gas Turbines Power. May 2008; Vol. 130, No. 3, 032504. DOI: 10.1115/1.2838995. Open DOISearch in Google Scholar

[18] Whitehead, D. S. (1988). The Maximum Factor by Which Forced Vibration of Blades Can Increase Due to Mistuning, ASME J. Eng. Gas Turbines Power, Vol. 120, No. 1, 115–119. Search in Google Scholar

eISSN:
2300-7591
Language:
English
Publication timeframe:
Volume Open
Journal Subjects:
Engineering, Introductions and Overviews, other