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Fail-Safe Structural Design

Published online by Cambridge University Press:  04 July 2016

W. T. Koiter
W. T. Koiter*
Affiliation:
Technological University, Delft
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Extract

MR. Harpur's interesting and stimulating paper (page 363, May 1958 Journal) is obviously of great importance to all who have to face the problem of fatigue strength of aircraft. These comments all refer to Section 3—Design Loads. Mr. Harpur's conclusions are based on analysis of a typical flight plan of a medium haul civil transport, and are formulated as a proposal for two fail-safe design requirements.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 62 , Issue 574 , October 1958 , pp. 757 - 760
Copyright
Copyright © Royal Aeronautical Society 1958

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