THE STATIC ANALYSIS OF COMPOSITE AIRCRAFT WINGBOX STRUCTURE
In this paper, the static analysis for finding the best location of boxes inside the composite wing-box structure has been performed. A software ANSYS (ver.11) was used to analyses the Aluminum wing to find the maximum stresses reached in. These results are used as a base for the composite wingbox...
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| 主要な著者: | , |
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| フォーマット: | Artigo |
| 言語: | Inglês |
| 出版事項: |
University of Baghdad
2011-12-01
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| シリーズ: | Journal of Engineering |
| 主題: | |
| オンライン･アクセス: | https://joe.uobaghdad.edu.iq/index.php/main/article/view/3026 |
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