【摘要】 本文对火箭弹气动弹性发散计算进行了较详细的研究,包括与气动弹性发散计算方法有关的结构质量—刚度模型、气动升力模型和安全裕度要求等。更多还原

【Abstract】 In this paper, the aeroelastic divergence computation of missile including the structure mass - rigidity model and the aerodynamic lift force model which relate to the computational method of areoelastic divergence, and safety margin requirement, is studied in detail.更多还原