NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Some approximations in the linear dynamic equations of thin cylindersTheoretical analysis is performed on the linear dynamic equations of thin cylindrical shells to find the error committed by making the Donnell assumption and the neglect of in-plane inertia. At first, the effect of these approximations is studied on a shell with classical simply supported boundary condition. The same approximations are then investigated for other boundary conditions from a consistent approximate solution of the eigenvalue problem. The Donnell assumption is valid at frequencies high compared with the ring frequencies, for finite length thin shells. The error in the eigenfrequencies from omitting tangential inertia is appreciable for modes with large circumferential and axial wavelengths, independent of shell thickness and boundary conditions.
Document ID
19810055515
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
El-Raheb, M.
(California Institute of Technology, Jet Propulsion Laboratory, Pasadena CA, United States)
Babcock, C. D., Jr.
(California Institute of Technology Pasadena, CA, United States)
Date Acquired
August 11, 2013
Publication Date
June 22, 1981
Publication Information
Publication: Journal of Sound and Vibration
Volume: 76
Subject Category
Structural Mechanics
Accession Number
81A39919
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available