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Explosive shock damage potential in space structuresThe effects of a pulse shape on the transient response of a cylindrical shell are presented. Uniaxial, membrane, and bending theories for isotropic shells were used in this study. In addition to the results of the analytical study, the preliminary results of an experimental study into the generation and measurement of shear waves in a cylindrical shell are included.
Document ID
19730006164
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mortimer, R. W. (Drexel Univ. Philadelphia, PA, United States)
Date Acquired
September 2, 2013
Publication Date
September 29, 1972
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-112221
Report Number: NASA-CR-112221
Accession Number
73N14891
Funding Number(s)
CONTRACT_GRANT: NGR-39-004-041
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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