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The Consideration of Internal Damping in the Two-Dimensional Problem of Wing Vibration*

Published online by Cambridge University Press:  28 July 2016

R. Kassner
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Extract

In conjunction with H. Fingado, the author has described a graphical method for the rapid determination of the critical velocity of a two-dimensional wing without damping (see L.F.F., Vol. 13, No. 11 (20/11/36), pp. 374-387). The present paper presents a continuation of this work taking into account internal damping of the wing.

Type
Research Article
Information
The Aeronautical Journal , Volume 41 , Issue 322 , October 1937 , pp. 945 - 952
Copyright
Copyright © Royal Aeronautical Society 1937

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Footnotes

*

Luftfahrtforschung, Vol. 13, No. 11, 20th Nov., 1936, pp. 388-390. Translated by the Aeronautical Research Committee (Oscillation Sub-Committee) and published by their permission and that of the author.

References

* Luftfahrtforschung, Vol. 13, No. 11, 20th Nov., 1936, pp. 388-390. Translated by the Aeronautical Research Committee (Oscillation Sub-Committee) and published by their permission and that of the author.