SCALING OF LOW-VELOCITY IMPACT FOR SYMMETRICAL COMPOSITE LAMINATES

被引:23
|
作者
SANKAR, BV
机构
[1] Department of Aerospace Engineering, Mechanics and Engineering Science, University of Florida Gainesville
关键词
SCALING OF IMPACT; LOW-VELOCITY IMPACT; COMPOSITE LAMINATES; NONDIMENSIONAL MODELS;
D O I
10.1177/073168449201100304
中图分类号
TB33 [复合材料];
学科分类号
摘要
The equations governing the problem of low-velocity impact of a simply supported rectangular midplane-symmetric laminated plate are nondimensionalized such that the problem is defined in terms of five dimensionless parameters. A parametric study using the Graeco-Latin Factorial Plan is performed. Semi-empirical formulas for maximum impact force, impact duration, and maximum back surface strains are obtained. It is found that some of the simple impact models provide the bounds for the case of impact on a finite extent plate. A one parameter model is derived for impacts of short duration.
引用
收藏
页码:296 / 309
页数:14
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