The Influence of Thermal Effects on the Design and Testing of Aircraft Structures

Strang, W. J.

doi:10.1177/0020348363178001158

Proceedings of the Institution of Mechanical Engineers

1963

DOI: 10.1177/0020348363178001158

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The Influence of Thermal Effects on the Design and Testing of Aircraft Structures

W. J. Strang¹

Abstract: These loads. are commonly referred to as gust loads.

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1969

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A Review of the Interaction of Creep and Fatigue

Ellison

1969

Journal of Mechanical Engineering Science

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hiany components in supersonic aircraft and modern power plant operate under cyclic conditions at increased temperatures at which creep processes also occur. Solving associated material problems depends, to a major extent, on understanding the various factors influencing behaviour, such as the effect of stress or strain cycling, dwell periods, temperature, notches, environment, multiaxial stress, ductility, and the effect of prior testing on subsequent endurance. T h e various methods of testing are briefly described and the mode of failure where there is interaction between creep and fatigue is discussed. Method5 for predicting deformation and life are also presented. Finally, the review concludes with suggestions for future work.

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A Review of the Interaction of Creep and Fatigue

Ellison

1969

Journal of Mechanical Engineering Science

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The Influence of Thermal Effects on the Design and Testing of Aircraft Structures

Abstract: These loads. are commonly referred to as gust loads.

Cited by 1 publication

References 2 publications

A Review of the Interaction of Creep and Fatigue

A Review of the Interaction of Creep and Fatigue

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