The effect of fuel weight distribution on the aeroelastic instability of swept wings
In this work, a study has been conducted to observe the influence of fuel weight distribution on the flutter characteristics of a high aspect ratio swept wing. In this paper, B777-200 wing model having a 34º sweptback angle is used as a baseline and two other models with the swept angles of 0º (stra...
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| Main Authors: | , , |
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| 格式: | Article |
| 语言: | English English |
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MechAero Foundation for Technical Research & Education Excellence (MAFTREE)
2020
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| 在线阅读: | http://irep.iium.edu.my/85963/1/Acceptance%20proof%20-%20Editor%20of%20the%20IJVSS%20journal.pdf http://irep.iium.edu.my/85963/2/IJVSS%20first%20page.pdf http://irep.iium.edu.my/85963/ https://maftree.org/eja/index.php/ijvss/index |
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