A finite element analysis of impact damage in composite laminates

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The Aeronautical Journal, Vol. 116, Iss. 1186, 2012-12 ,pp. : 1331-1347

Cambridge University Press

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Predicting low-velocity impact damage in composites by a quasi-static load model with cohesive interface elements

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The Aeronautical Journal, Vol. 116, Iss. 1186, 2012-12 ,pp. : 1367-1381

Cambridge University Press

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An application of a new ultrasonic technique to jute composite laminates subjected to low-velocity impact

By Scarponi C.   Valente M.  

International Journal of Materials and Product Technology, Vol. 26, Iss. 1-2, 2006-02 ,pp. : 6-18

Inderscience Publishers

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Modelling of impact damage zones in composite laminates for strength after impact

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The Aeronautical Journal, Vol. 116, Iss. 1186, 2012-12 ,pp. : 1349-1365

Cambridge University Press

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Analysis of factors influencing deflection in sandwich panels subjected to low-velocity impact

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The International Journal of Advanced Manufacturing Technology, Vol. 52, Iss. 5-8, 2011-02 ,pp. : 433-441

Springer Publishing Company

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