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The solution of large flutter problems on small computers
Published online by Cambridge University Press: 04 July 2016
Summary
The ‘inverse method’ proposed in 1936 by Duncan, Collar and Lyon for the calculation of flutter boundaries is re-stated in a form suited to modern methods of dynamical and numerical analysis and programmed for use on a home computer. The method is extended to provide information on sub- and supercritical eigenvalues. For a microcomputer with 32K RAM, flutter problems of orders up to 35 may be accurately solved.
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- Research Article
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- Copyright © Royal Aeronautical Society 1984
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