Static fracture and modal analysis simulation of a gas turbine compressor blade and bladed disk system

Author:

Fernandes Ralston,El-Borgi Sami,Ahmed Khaled,Friswell Michael I.,Jamia Nidhal

Publisher

Springer Science and Business Media LLC

Subject

Applied Mathematics,Computer Science Applications,Engineering (miscellaneous),Modelling and Simulation

Reference20 articles.

1. Meher-Homji B, Gabriles G. Gas turbine blade failures–causes avoidance and troubleshooting. In: Proceedings of the 27th Turbomachinery Symposium. Texas A&M University, College Station, Texas. 1998, pp. 129–80.

2. Witek L. Simulation of crack growth in the compressor blade subjected to resonant vibration using hybrid method. Eng Fail Anal. 2015;49:57–66.

3. Poursaeidi E, Bakhtiari H. Fatigue crack growth simulation in a first stage of compressor blade. Eng Fail Anal. 2014;45:314–25.

4. Wawrzynek PA, Carter BJ, Ingraffea AR. Advances in simulation of arbitrary 3D crack growth using FRANC3D/NG. In: Proceedings of the 12th International Congress on Fracture ICF12. Ottawa. 2009, pp. 344–354.

5. Newman JC, Raju IS. An empirical stress-intensity factor equation for the surface crack. Eng Fract Mech. 1981;15(1–2):185–92.

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