Modal and Aeroelastic Analysis of A High-Aspect-Ratio Wing with Large Deflection Capability
This paper describes a modified structural dynamics model for aeroelastic analysis of high-aspect-ratio wings undergoing large deformation behavior. To gain this aim, a moderate deflection beam model is modified with some important large deflection terms and then coupled with a state space unsteady...
محفوظ في:
| المؤلفون الرئيسيون: | , , |
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| التنسيق: | Artigo |
| اللغة: | Inglês |
| منشور في: |
Islamic Azad University-Isfahan (Khorasgan) Branch
2015-03-01
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| سلاسل: | International Journal of Advanced Design and Manufacturing Technology |
| الموضوعات: | |
| الوصول للمادة أونلاين: | https://admt.isfahan.iau.ir/article_534915_1b27d7674d1a0bf8429c62ae18632df5.pdf |
| الوسوم: |
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