Modern Methods of Investigating Flutter and Vibration

Author:

Hitch H. P. Y.

Abstract

SummaryThe past several years have seen a steady advance in the techniques employed in flutter and vibration analysis. At the same time aircraft performance has been improved on every front and margins have had to be reduced: it is only by making full use of these modern methods that the accepted margins of safety have been preserved.The paper reviews the processes which are currently used in the prediction and prevention of aircraft flutter in contrast to those of a few years back. The more recent types of flutter which have had to be considered are discussed briefly in relation to the methods which have been developed to deal with them. Ground and Flight testing methods are reviewed together with the use to which the results are put.Finally there is a discussion of the increasing need to predict sub-critical response. The methods employed are discussed in relation to the more important problems.

Publisher

Cambridge University Press (CUP)

Reference20 articles.

1. Fung Y. A Summary of the Theories and Experiments on Panel Flutter. GALCIT AFOSR TN 60-224, May 1960.

2. The Second Lanchester Memorial Lecture

3. An investigation into the theory of resonance testing

4. Jones W. P. Aerodynamic Forces on Wings in Non-Uniform Motion. R & M 2117, August 1945.

5. Bellerby P. A Note on In-Flight Flutter Testing using the Method of Decaying Oscillations. Blackburn Aircraft Ltd. Note YFT 1683, October 1959 (unpublished).

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