Structural comparison of vertical and horizontal layout of carrying arms of rotary-wing UAV with finite element analysis
In this study, numerical analysis of the fuselage of a rotary wing unmanned aerial vehicle was conducted. A fuselage that is resistant to the loads on the fuselage and has maximum lightness has been designed. In this context, the fuselage design was conducted based on the loads that the aircraft's f...
সংরক্ষণ করুন:
| প্রধান লেখক: | , , , |
|---|---|
| বিন্যাস: | Artigo |
| ভাষা: | Inglês |
| প্রকাশিত: |
Ahmet Çalık
2023-06-01
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| মালা: | European Mechanical Science |
| বিষয়গুলি: | |
| অনলাইন ব্যবহার করুন: | https://dergipark.org.tr/en/download/article-file/2918590 |
| ট্যাগগুলো: |
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