建立了带柔性后缘自适应机翼模型和带刚性偏转后缘的传统机翼模型，从升阻特性和力矩特性以及操纵效率对它们进行了比较研究。
This paper aims at presenting an investigation into aerodynamics and control reversal characteristics of adaptive wings with seamless, variable camber, flexible trailing edge.
传统机身设计要求使用重型结构材料，以便把机身横向重量转移到机翼下方的起落架和机轮上。
Conventional airframes require heavy structural material to transfer the fuselage's weight laterally to landing gear and wheels under the wings.
先进的混合机翼体，用三角造型代替了传统的管型。
The leading contender is the fabled blended-wing body, which replaces the conventional tube with a triangular shape.
随着现代机翼整体壁板设计水平的不断提高，传统的制造模式已不能满足其制造要求。
With the development of integral wing panel design, conventional manufacture mode of integral panel can not satisfy modern manufacturing requirement.
讨论了一种区别于机翼与圆柱机身的传统民机外形——翼身融合体(BWB)外形。
A new type of transport, which is different from the conventional cylinder fuselage plus wing but a blended wing body (BWB), is discussed.
讨论了一种区别于机翼与圆柱机身的传统民机外形——翼身融合体(BWB)外形。
A new type of transport, which is different from the conventional cylinder fuselage plus wing but a blended wing body (BWB), is discussed.
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