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。
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.
出处
《强度与环境》
2003年第3期39-42,共4页
Structure & Environment Engineering
