کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
510513 | 865769 | 2007 | 12 صفحه PDF | دانلود رایگان |
عنوان انگلیسی مقاله ISI
Optimum design of composite plate wings for aeroelastic characteristics using lamination parameters
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کلمات کلیدی
موضوعات مرتبط
مهندسی و علوم پایه
مهندسی کامپیوتر
نرم افزارهای علوم کامپیوتر
پیش نمایش صفحه اول مقاله
![عکس صفحه اول مقاله: Optimum design of composite plate wings for aeroelastic characteristics using lamination parameters Optimum design of composite plate wings for aeroelastic characteristics using lamination parameters](/preview/png/510513.png)
چکیده انگلیسی
The present paper treats the flutter and divergence characteristics of composite plate wings with various sweep angles. First, the effect of laminate configuration on the flutter and divergence characteristics is investigated for composite plate wings. To examine the effect of laminate configuration, the flutter and divergence characteristics are represented on the lamination parameter plane. Next, a minimum weight design of composite plate wings subjected to the constraints on the flutter and divergence speeds is conducted by using a genetic algorithm in which lamination parameters are used as design variables. The effectiveness of aeroelastic tailoring is demonstrated through the optimization results.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Computers & Structures - Volume 85, Issues 3–4, February 2007, Pages 213–224
Journal: Computers & Structures - Volume 85, Issues 3–4, February 2007, Pages 213–224
نویسندگان
Masaki Kameyama, Hisao Fukunaga,