Automated Finite Element Modeling Of Wing Structures For Shape Optimization
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Automated Finite Element Modeling Of Wing Structures For Shape Optimization
The Displacement Formulation Of The Finite Element Method Is The Most General And Most Widely Technique For Structural Analysis Of Airplane Configurations. Modem Structural Synthesis Techniques Based On The Finite Element Method Have Reached A Certain Maturity In Recent Years, And Large Airplane Structures Can Now Be Optimized With Respect To Sizing Type Design Variables For Many Load Cases Subject To A Rich Variety Of Constraints Including Stress, Buckling, Frequency, Stiffness And Aeroelastic Constraints (refs. 1-3).
- 品牌: Creative Media Partners, LLC
- 类别: 计算机与互联网
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语言: English
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作者: Creative Media Partners LLC
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出版日期: 2025-06-13
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页数: 184
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出版社／标签: Creative Media Partners | LLC
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格式: Paperback
- Fruugo ID: 557022045-1125287368
- ISBN: 9781288910045
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