摘要: This paper considers the aeroelastic optimization of a subsonic transport wingbox under a variety of static and dynamic aeroelastic constraints. Three types of design variables are utilized: structural variables (skin thickness, s... 展开
作者 | Stanford, B. K. | ||
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原报告号 | N160006015 | 总页数 | 19 |
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 | Design analysis Wings Aeroservoelasticity Aeroelasticity Subsonic aircraft Control surfaces Aircraft design Flutter Linear quadratic regulator Aerodynamic loads Structural design Airspeed Static loads Design optimization |