A theoretical analysis of the free vibration of discretely stiffened cylindrical shells with arbitrary end conditions / by D.M. Egle and K.E. Soder.

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Bibliographic Details
Online Access:	Search for the full-text version of this title in HathiTrust
Main Author:	Egle, D. M.
Corporate Authors:	United States. National Aeronautics and Space Administration, Langley Research Center, University of Oklahoma
Other Authors:	Soder, K. E.
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1969.
Series:	NASA contractor report ; NASA CR-1316.
Subjects:	Cylindrical shells. Free vibration. Rayleigh-ritz method. Stiffness. Computer programs. Digital computers. Flexibility. Stiffening. Vibration effects. Cylindric algebras. Vibration (Aeronautics)

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Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.26:1316
NAS 1.26:1316	Available Place a Hold