Estimation of Residual Life and Failure Mechanism of Cracked Aircraft Wing Skin
Author:
Publisher
Springer Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-15-4779-9_33
Reference17 articles.
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3. Vashisht KV (2016) Damage tolerance evaluation of an aircraft skin structure by MVCCI technique (2d analysis) using MSC–Nastran/Patran. Int J Res Eng Technol 5:510–516
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5. Elisa P (2011) Virtual crack closure technique and finite element method for predicting the delamination growth initiation in composite structures. In: Advances in composite materials-analysis of natural and man-made materials. IntechOpen
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