UAV NACA4415 wing structural performance analysis subjected to external aerodynamic load using Schrenk’s approximation
Structural analysis is widely used in the analysis of aircraft structures with the common application of the finite element method. The optimum structural design of aircraft wing is the crucial aspect in the performance of the aircraft considering the high stiffness-to-weight...
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| 主要な著者: | , , , , , |
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| フォーマット: | 論文 |
| 言語: | English |
| 出版事項: |
Penerbit Akademia Baru
2019
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| オンライン･アクセス: | http://psasir.upm.edu.my/id/eprint/82455/1/UAV%20NACA4415%20wing%20.pdf http://psasir.upm.edu.my/id/eprint/82455/ https://akademiabaru.com/submit/index.php/arfmts/article/view/2642 |
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