Damage analysis of honeycomb core composite sandwich plate subjected low velocity impact

Journal of Reinforced Plastics and Composites

Volumn 19, Issue 1, 2000, Pages 58-68

  Zheng, Qixuan ^a   Li, Zhengneng ^a   Wu, Di ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

[No Author keywords available]

Indexed keywords

FINITE ELEMENT METHOD; HONEYCOMB STRUCTURES; IMPACT TESTING; MATHEMATICAL MODELS; SANDWICH STRUCTURES; STRUCTURAL ANALYSIS;

DAMAGE ANALYSIS; DAMAGE EXTENSION CRITERIA; DAMAGE OCCURRING CRITERIA;

PLATES (STRUCTURAL COMPONENTS);

EID: 0033887598     PISSN: 07316844     EISSN: None     Source Type: Journal    
DOI: 10.1106/JV4W-N0EF-NJLF-JFPU     Document Type: Article

References (3)

1. Choi H. Y. and Chang F. K., A Model for Predicting Damage in Graphite/Epoxy Laminated Composites Resulting from Low Velocity Point Impact, J of Composite Materials, 1992, 26(14):2134-2169.
2. Hertz H., Uber Die Beruhrung Fester Elastischer Korper, J of Reine Angle Math, Crelle, Vol. 1992, pp 155.
3. Yang S.H. and Sun C.T., Indentation Law for Composite Laminates, ASTM STP 787 American Society for Testing and Materials, 1982, pp. 425-449.