NASA NTRS · 19750031889
Reanalysis information for eigenvalues derived from a differential equation analysis formulation
Abstract
The investigation reported demonstrates that in the case considered perturbation methods can be used in a straightforward manner to obtain reanalysis information. A perturbation formula for the buckling loads of a general shell of revolution is derived. The accuracy of the obtained relations and their range of application is studied with the aid of a specific example involving a particular stiffened shell of revolution.
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Thornton, W. A., Majumder, D. K.. 1974-12-01. Reanalysis information for eigenvalues derived from a differential equation analysis formulation. https://ntrs.nasa.gov/citations/19750031889
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