Issues of multidisciplinary design are considered in view of the aerodynamical and structural design of the airframe, i. e. fuselage, wing, and tail unit. Background problems, like Cayley's design paradigm are discussed, as well as ideal-typical airframe definition and development phases, and the industrial challenges which numerical multidisciplinary design and optimization (MDSO) poses. Finally the state of the art of MDSO methods is illustrated.


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