Abstract
High temperature components assembled in aircraft turbines are subjected to complex stress, including thermal stress, stress originating from centrifugal force and high frequency vibration stress. Recently increased attention has been paid to the study of creep and fatigue interaction which appears to be an important factor in the prediction of the components’ life1,2.
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© 1996 Plenum Press, New York
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Zrník, J., Wang, Z.G., Yu, Y., Wang, J.A., Žitňanský, M., Horňak, P. (1996). Cyclic Creep Deformation Characteristics Of Single Crystal Of Nickle Basesuperalloy CMSX 3. In: Gonis, A., Turchi, P.E.A., Kudrnovský, J. (eds) Stability of Materials. NATO ASI Series, vol 355. Springer, Boston, MA. https://doi.org/10.1007/978-1-4613-0385-5_50
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DOI: https://doi.org/10.1007/978-1-4613-0385-5_50
Publisher Name: Springer, Boston, MA
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