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    Effect of Boundary Condition on Numerical Study of UAV Composite Skin Panels Under Dynamic Impact Loading

    Effect of Boundary Condition on Numerical Study of UAV Composite Skin Panels Under Dynamic Impact Loading by Ilham Bagus Wiranto, Sherly Octavia Saraswati, Iqbal Reza Alfikri, Chairunnisa Chairunnisa, Fadli Cahya Megawanto, Muhammad Ilham Adhynugraha, Nur Cholis Majid

    Published 2024-03-01
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