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Vibration response of geometrically nonlinear elastic beams to pulse and impact loadingThe governing equations for the geometrically nonlinear deformation of elastic beams subjected to dynamic bending loads are developed and solved for various initial conditions. Of primary interest is the response to pulse loading and simulated impact. Both transient and several cycle solutions are generated for the free vibration response to pulse loading. The results obtained are compared to a first mode analysis approximation. A model is developed to simulate impact loading by the distribution of additional mass to the elastic system and subjecting it to a velocity pulse. The governing equations are solved using second order finite differences in space and time. The solutions obtained are in reasonable agreement with experimental results.
Document ID
19840004459
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Liebowitz, H.
(George Washington Univ. Washington, DC, United States)
Date Acquired
September 4, 2013
Publication Date
October 7, 1983
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-174495
NAS 1.26:174495
Report Number: NASA-CR-174495
Report Number: NAS 1.26:174495
Accession Number
84N12527
Funding Number(s)
CONTRACT_GRANT: NAG1-158
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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