李永强，李锋，何永亮.四边固支铝基蜂窝夹层板弯曲自由振动分析［J］.复合材料学报，2011，28(3):210-216.(Li Yong-qiang，Li Feng，He Yong-liang.Flexural vibration analysis of honeycomb sandwich plate with completely clamped support［J］.Acta Materiae Compositae Sinica，2011，28(3):210-216.)
[2]
管公顺，庞宝君，崔乃刚，等.铝球弹丸超高速正撞击薄铝板穿孔尺寸研究［J］.工程力学，2007，24(12):181-185.(Guan Gong-shun，Pang Bao-jun，Cui Nai-gang，et al.Size investigation of hole due to hypervelocity impact aluminum spheres on thin aluminum sheet［J］.Engineering Mechanics，2007，24(12):181-185.)
[3]
何永亮.低速冲击下蜂窝夹层板损伤标识量的提取研究［D］.沈阳:东北大学，2011.(He Yong-liang.Study on damage detection of honeycomb sandwich plate with low velocity impact damage［D］.Shenyang:Northeastern University，2011.)
[4]
Fleck A N，Deshpande S V.The resistance of clamped sandwich beams to shock loading［J］.Journal of Applied Mechanics，2004，71(3):386-401.
[5]
Schonberg W P，Mohamed E.Analytical hole diameter and crack length models for multi-wall systems under hypervelocity projectile impact［J］.International Journal of Impact Engineering，1993，23(1):835-864.
[6]
Sawle D R.Hypervelocity impact in thin sheets，semi- infinite targets at 15km/s［C］// AIAA Hypervelocity Impact Conference.Cincinnati，1969:69-378
[7]
Maiden C J，McMillan A R.An investigation of the protection afforded a spacecraft by a thin shield［J］.AIAA Journal，1964，2(11):1992-1998.
[8]
Nysmith C R，Denardo B P.Experimental investigations of momentum transfer associated with impact into thin alumi-num targets［R］.NASA TND-5492.Washington，DC，1969.
[9]
Hutchinson J W，Xue Z.Metal sandwich plates optimized for pressure impulses［J］.International Journal of Mechanical Sciences，2005，47(4):545-569.
[10]
Xue Z，Hutchinson J W.A comparative study of impulse-resistant metal sandwich plates［J］ .International Journal of Impact Engineering，2004，30(10):1283-1305.
[11]
宋延泽.泡沫铝子弹撞击下多孔金属夹芯板的塑性动力响应研究［D］.太原:太原理工大学，2009.(Song Yan-ze.Investigation on plastic dynamic response of sandwich plates with cellular metallic materials subjected to foam aluminium projectile impacting［D］.Taiyuan:Taiyuan University of Technology，2009)
