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Volume 21, Issue 2
1 February 1949
This article was originally published in
Aircraft Engineering
Aircraft Engineering Cover Image for Volume 21, Issue 2
Review Article| February 01 1949

A Note on Natural Frequencies: Natural Frequencies of Uncoupled Flexural and Torsional Oscillations with Damping of a Cantilever Wing Available to Purchase

M.Z. Krzywoblocki, Dr.Ae.E., M.A., M.Sc, M.Ae.E., Dipl.‐lng., A.F.R.Ae.S., A.F.I.Ae.S.
M.Z. Krzywoblocki, Dr.Ae.E., M.A., M.Sc, M.Ae.E., Dipl.‐lng., A.F.R.Ae.S., A.F.I.Ae.S.
Associate Professor of Aeronautical Engineering, University of Illinois, Urbana, Illinois, U.S.A.
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Author & Article Information
Publisher: Emerald Publishing
Online ISSN: 2059-9366
Print ISSN: 0002-2667
© MCB UP Limited
1949
Aircraft Engineering (1949) 21 (2): 49–54.
https://doi.org/10.1108/eb031727

THE aim of this paper is to calculate the natural frequencies and to consider the influence of the damping parameter on a wing's natural flexural and torsional vibration. The author took into account only the elastic hysteresis of the material because the structural damping, depending on the type of the aeroplane, cannot be taken into account in a general consideration.

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© MCB UP Limited
1949
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