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Publisher: Wiley-Blackwell

Volume 31, Number 6, June 2008

Thermoelastic investigation of an aluminium helicopter component under non-adiabatic conditions
pp. 405-413(9)
Authors: GALLOTTI, A.; SALERNO, A.; DESIDERATI, S.; FANTONI, G.

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Life assessment of multiaxially cyclic loaded turbine components
pp. 441-451(11)
Authors: RAUCH, M.; ROOS, E.

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Modelling fatigue crack propagation in CT specimens
pp. 452-465(14)
Authors: BRANCO, R.; ANTUNES, F. V.; MARTINS, R. F.

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Fatigue crack initiation in hardened medium carbon steel due to manganese sulphide inclusion clusters
pp. 466-477(12)
Authors: TEMMEL, C.; KARLSSON, B.; INGESTEN, N.-G.

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