Static Analysis of 3D-Printed Sub Wing Box Lug Joint Assembly using Finite Element Method

Today, 3D printing equipment is reasonably priced and widely available. This allows for the design creation of more complex structures for aerospace applications, especially for the unmanned aerial vehicle (UAV). In this study, a simulated 3D-printed airframe has been evaluated for use with a blende...

وصف كامل

التفاصيل البيبلوغرافية
الحاوية / القاعدة:Journal of Aeronautics, Astronautics and Aviation
المؤلف الرئيسي: 2-s2.0-85132112562
التنسيق: مقال
اللغة:English
منشور في: The Aeronautical and Astronautical Society of the Republic of China 2022
الوصول للمادة أونلاين:https://www.scopus.com/inward/record.uri?eid=2-s2.0-85132112562&doi=10.6125%2fJoAAA.202209_54%283%29.10&partnerID=40&md5=07a7f87cab17385d83f9b4af7412f912