Impact Response of Carbon Fiber Sandwich Panels with Honeycomb Core by using Experimental, Numerical and Analytical Methods

n this study, the low-and high-velocity impact behavior of carbon fiber composite sandwich panels was investigated using numerical, experimental, and analytical methods. The damage mechanism on the sandwich panel was investigated in terms of ballistic limit,...

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التفاصيل البيبلوغرافية

الحاوية / القاعدة:	Havacılık ve Uzay Teknolojileri Dergisi
المؤلفون الرئيسيون:	Mustafa Bilgin, Beyza Sül, Tutku Özkan, Uğur Yolum, Halit Süleyman Türkmen, Fatih Usta
التنسيق:	مقال
اللغة:	الإنجليزية
منشور في:	Turkish Air Force Academy 2025-07-01
الموضوعات:	composite materials sandwich panels honeycombs impact resistance
الوصول للمادة أونلاين:	https://jast.hho.msu.edu.tr/index.php/JAST/article/view/623