Structural response of composite sandwich panels impacted with and without compression loading

被引:7
作者
McGowan, DM [1 ]
Ambur, DR [1 ]
机构
[1] NASA, Langley Res Ctr, Struct Mech Branch, Hampton, VA 23681 USA
来源
JOURNAL OF AIRCRAFT | 1999年 / 36卷 / 03期
关键词
D O I
10.2514/2.2476
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The results of an experimental study of the impact damage characteristics and residual strength of composite sandwich panels impacted with and without a compression lending are presented. Results of impact damage screening tests conducted to identify the impact-energy levels at which damage initiates and barely visible impact damage occurs in the impacted facesheet are discussed. Parametric effects studied in these tests include the impactor diameter and dropped-weight vs airgun-launched impactors. Residual strength results of panels tested in compression after impact are presented and compared with results of panels that are subjected to a compressive preload prior to being impacted.
引用
收藏
页码:596 / 602
页数:7
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