A new method for evaluating the residual compression strength of composites after impact

Composite Structures

Volumn 53, Issue 3, 2001, Pages 309-316

  Habib, F A ^a  

^a BAE SYSTEMS   (United Kingdom)

Author keywords

CAI; Composites; Impact

Indexed keywords

BUCKLING; COMPRESSIVE STRENGTH; CORRELATION METHODS; FINITE ELEMENT METHOD; STRUCTURAL PANELS;

COMPRESSION PANELS;

AIRCRAFT MATERIALS;

AEROSPACE TEXTILE; COMPOSITE PROPERTY; COMPRESSIVE PROPERTY; IMPACT; STRENGTH; TESTING;

EID: 0035423562     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(01)00015-0     Document Type: Article

References (6)

1. Effect of impact on the compressive response of FRP composite laminates
2. Residual compression strength of composites after impact
3. EFA damage tolerance programme
4. Residual compression strength of composites after impact