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The Principles Underlying the Dynamic Stressing of Aeroplanes*

Published online by Cambridge University Press:  28 July 2016

D. Williams
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Extract

The purpose of this paper is to explain the principles governing the behaviour of structures under transient dynamic loads, such as those encountered by aircraft structures during landing or flying in gusty weather. The paper is intended mainly for the young aeronautical engineer who may not be particularly well versed in this aspect of stress work.

Type
Research Article
Information
The Aeronautical Journal , Volume 55 , Issue 486 , June 1951 , pp. 362 - 381
Copyright
Copyright © Royal Aeronautical Society 1951

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Footnotes

*

This paper is the basis of a Lecture given to the Southampton Branch of the Society on 1st November 1950.

References

Note on Page 374 * This assumed numerical value for the slope of the lift curve is the one most open to uncertainty in this estimate of wing aerodynamic damping.