摘要: This work explores the use of alternative internal structural designs within a full-scale wing box structure for aeroelastic tailoring, with a focus on curvilinear spars, ribs, and stringers. The baseline wing model is a fully-pop... 展开
作者 | Jutte, C. V. Stanford, B. K. Wieseman, C. D. | ||
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原报告号 | N150003788 | 总页数 | 48 |
主办者 | National Aeronautics and Space Administration | ||
报告分类号 | [51C - Aircraft, 51F - Test Facilities &, Equipment] | ||
报告类别/文献类型 | DE / NTIS科技报告 | ||
关键词 | Wings Structural design Dynamic structural analysis Aeroelasticity Aircraft design Reinforcement (structures) Ribs (supports) Stringers Leading edges Weight reduction Flutter analysis Nastran Design analysis Design optimization |