How to cite this paper
Nakhodchi, S & Maman, E. (2014). Fatigue life prediction in the damaged and un-damaged compressor blades.Engineering Solid Mechanics, 2(1), 43-50.
Refrences
Dowling, N. E. (1999). Mechanical behavior of materials: engineering methods for deformation, fracture, and fatigue (pp. 562-570). Upper Saddle River^ eNJ NJ: prentice Hall.
Farrahi, G. H., Tirehdast, M., Masoumi Khalil Abad, E., Parsa, S., & Motakefpoor, M. (2011). Failure analysis of a gas turbine compressor.Engineering Failure Analysis, 18(1), 474-484.
Frankel, P. G., Withers, P. J., Preuss, M., Wang, H. T., Tong, J., & Rugg, D. (2012). Residual stress fields after FOD impact on flat and aerofoil-shaped leading edges. Mechanics of Materials. 55: 130–145.
Infante, V., Silva, J. M., de Freitas, M., & Reis, L. (2009). Failures analysis of compressor blades of aeroengines due to service. Engineering Failure Analysis,16(4), 1118-1125.
Kermanpur, A., Sepehri Amin, H., Ziaei-Rad, S., Nourbakhshnia, N., & Mosaddeghfar, M. (2008). Failure analysis of Ti6Al4V gas turbine compressor blades. Engineering Failure Analysis, 15(8), 1052-1064.
Nowell, D., Duo, P., & Stewart, I. F. (2003). Prediction of fatigue performance in gas turbine blades after foreign object damage. International journal of fatigue,25(9), 963-969.
Poursaeidi, E., Aieneravaie, M., & Mohammadi, M. R. (2008). Failure analysis of a second stage blade in a gas turbine engine. Engineering Failure Analysis,15(8), 1111-1129.
Poursaeidi, E., Babayee, A., Behrouzshad, F., & Mohammadi Arhani, M. R. (2012). Failure analysis of an axial compressor first row rotating blades.Engineering Failure Analysis.
Ruschau, J. J., Nicholas, T., & Thompson, S. R. (2001). Influence of foreign object damage (FOD) on the fatigue life of simulated Ti-6Al-4V airfoils. International journal of impact engineering, 25(3), 233-250.
Tsai, G. C. (2004). Rotating vibration behavior of the turbine blades with different groups of blades. Journal of sound and vibration, 271(3), 547-575.
Witek, L. (2011). Crack propagation analysis of mechanically damaged compressor blades subjected to high cycle fatigue. Engineering Failure Analysis, 18(4), 1223-1232.
Witek, L., Wierzbi?ska, M., & Pozna?ska, A. (2009). Fracture analysis of compressor blade of a helicopter engine. Engineering Failure Analysis, 16(5), 1616-1622.
Farrahi, G. H., Tirehdast, M., Masoumi Khalil Abad, E., Parsa, S., & Motakefpoor, M. (2011). Failure analysis of a gas turbine compressor.Engineering Failure Analysis, 18(1), 474-484.
Frankel, P. G., Withers, P. J., Preuss, M., Wang, H. T., Tong, J., & Rugg, D. (2012). Residual stress fields after FOD impact on flat and aerofoil-shaped leading edges. Mechanics of Materials. 55: 130–145.
Infante, V., Silva, J. M., de Freitas, M., & Reis, L. (2009). Failures analysis of compressor blades of aeroengines due to service. Engineering Failure Analysis,16(4), 1118-1125.
Kermanpur, A., Sepehri Amin, H., Ziaei-Rad, S., Nourbakhshnia, N., & Mosaddeghfar, M. (2008). Failure analysis of Ti6Al4V gas turbine compressor blades. Engineering Failure Analysis, 15(8), 1052-1064.
Nowell, D., Duo, P., & Stewart, I. F. (2003). Prediction of fatigue performance in gas turbine blades after foreign object damage. International journal of fatigue,25(9), 963-969.
Poursaeidi, E., Aieneravaie, M., & Mohammadi, M. R. (2008). Failure analysis of a second stage blade in a gas turbine engine. Engineering Failure Analysis,15(8), 1111-1129.
Poursaeidi, E., Babayee, A., Behrouzshad, F., & Mohammadi Arhani, M. R. (2012). Failure analysis of an axial compressor first row rotating blades.Engineering Failure Analysis.
Ruschau, J. J., Nicholas, T., & Thompson, S. R. (2001). Influence of foreign object damage (FOD) on the fatigue life of simulated Ti-6Al-4V airfoils. International journal of impact engineering, 25(3), 233-250.
Tsai, G. C. (2004). Rotating vibration behavior of the turbine blades with different groups of blades. Journal of sound and vibration, 271(3), 547-575.
Witek, L. (2011). Crack propagation analysis of mechanically damaged compressor blades subjected to high cycle fatigue. Engineering Failure Analysis, 18(4), 1223-1232.
Witek, L., Wierzbi?ska, M., & Pozna?ska, A. (2009). Fracture analysis of compressor blade of a helicopter engine. Engineering Failure Analysis, 16(5), 1616-1622.