后掠

• Secondly , the static aeroelastic problems and jig - shape design , as a kind of multi - disciplinary design optimization ( mdo ) , are investigated for sweep wing and super - critical wing . numerical results are in good agreement with other reference data . the method and the program presented in this paper are verified
  分别以某后掠机翼和超临界机翼为算例，对机翼的静气动弹性问题以及基于静气动弹性的型架外形优化设计和飞行姿态确定进行研究，计算结果和有关文献的结果进行了比较，吻合很好。