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On the response of curved laminated panels subjected to transverse impact loads

✍ Scribed by Laura S Kistler; Anthony M Waas


Publisher
Elsevier Science
Year
1999
Tongue
English
Weight
622 KB
Volume
36
Category
Article
ISSN
0020-7683

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✦ Synopsis


Using static response characteristics as a tool for understanding impact response\ the in~uence of in!plane and out!of!plane boundary conditions\ the e}ect of curvature\ and the validity of linear and nonlinear plate theory are investigated for the transverse central impact on thin _ber reinforced composite cylindrical panels[ Comparisons between the force!deformation curves of a low velocity impact response and static problem are made[ These curves illustrate the importance of nonlinear e}ects on the large deformation response\ including the in~uence of curvature[ The static response is a lower limit to the impact response and\ for the present circumstances\ can give insight into low velocity impact response behavior[ Þ 0887 Elsevier Science Ltd[ All rights reserved[ Corresponding author[ 0 Graduate Research Assistant\ currently with Boeing Commercial Airplane company\ Seattle[ 1 Associate Professor[


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