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低阻、大升阻比的超音速飞行器乘波体的研究与发展日益受到各国空气动力学专家、学者的关注。依据已有资料，简要综述了乘波体外形的概念和特点，以及在超音速飞行器特别是现代导弹设计中的有关因素和应用前景。
The research and development of multiply body of supersonic aircraft with low resistance and high resistance ratio are increasingly concerned by aerodynamics experts and scholars in various countries. Based on the available data, the paper summarizes the concept and characteristics of the shape of multiplication body and the relevant factors and application prospects in the design of supersonic aircraft, especially modern missiles.