A model for compression after impact strength evaluationOne key property commonly used for evaluating composite material performance is compression after impact strength (CAI). Standarad CAI tests typically use a specific laminate stacking sequence, coupon geometry, and impact level. In order to understand what material factors affect CAI, evaluation of test results should include more than comparisons of the measured strength for different materials. This study considers the effects of characteristic impact damage state, specimen geometry, material toughness, ply group thickness, undamaged strength, and failure mode. The results of parametric studies, using an analysis model developed to predict CAI, are discussed. Experimental results used to verify the model are also presented. Finally, recommended pre- and post-test CAI evaluation schemes which help link material behavior to structural performance are summarized.
Document ID
19900046030
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ilcewicz, Larry B. (Boeing Co. Seattle, WA, United States)
Dost, Ernst F. (Boeing Co. Seattle, WA, United States)
Coggeshall, Randy L. (Boeing Co. Seattle, WA, United States)