aerodynamic influence coefficient造句

• Moreover , in the application of aircraft structures design , the composite wing is still to meet the needs of aeroelastic design . through reading the aerodynamic influence coefficient matrix from the nastran file , this paper generates a static aeroelastic equilibrium equation and divergence eigen - equation , which is needed by the aeroelastic tailoring of composite wing . through this equation , the aeroelastic tailoring of composite wing and its optimization design have come into being
  此外在飞机结构设计过程中，复合材料翼面结构还要满足气动弹性设计的需要，本文通过读入由nastran所产生的气动影响系数矩阵，构造出满足复合材料气动弹性分析所需要的静气动弹性平衡方程和发散特征方程，并在此基础上实现了复合材料气动弹性剪裁优化设计。