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Application of the dynamic stiffness method to the free and forced vibrations of aircraft panels

โœ Scribed by R.S. Langley


Publisher
Elsevier Science
Year
1989
Tongue
English
Weight
903 KB
Volume
135
Category
Article
ISSN
0022-460X

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๐Ÿ“œ SIMILAR VOLUMES


THE DYNAMIC STIFFNESS MATRIX METHOD IN F
โœ N.T. KHIEM; T.V. LIEN ๐Ÿ“‚ Article ๐Ÿ“… 2002 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 356 KB

The dynamic behaviour of a beam with numerous transverse cracks is studied. Based on the equivalent rotational spring model of crack and the transfer matrix for beam, the dynamic sti!ness matrix method has been developed for spectral analysis of forced vibration of a multiple cracked beam. As a part

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Starting from the governing di!erential equations of motion in free vibration, the dynamic sti!ness matrix of a uniform rotating Bernoulli}Euler beam is derived using the Frobenius method of solution in power series. The derivation includes the presence of an axial force at the outboard end of the b