An Investigation of Damage and Residual Strength of Aircraft Composite Structure Caused by Foreign Object Debris Impact
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-99-6030-9_40
Reference17 articles.
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3. Ashwin RK, Xiaodong X, David N, Michael RW, Stephen RH (2019) Experimental investigation of high velocity oblique impact and residual tensile strength of carbon/epoxy laminates. Compos Sci Tech 182:107772
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5. Cantwell WJ, Morton J (1989) Comparison of the low and high velocity impact response of CFRP. Composites 20:545–551
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