The research object of this paper is the static aeroelastic load correction method of civil aircraft.On the basis of fully considering the design characteristics and load correction requirements of modern civil aircraft with high aspect ratio,the existing static aeroelastic load correction method based on the aerodynamic theory of engineer-ing beams and strips is supplemented and improved,and a complete design flow and calculation method is estab-lished.The method is verified by the wind tunnel test data.Numerical examples show that the method is efficient and accurate,and has high engineering application value.
关键词
弹性变形/载荷分布/静气弹/载荷修正/风洞试验
Key words
elastic deformation/load distribution/static areoelasticity/load correction/wind tunnel test
维普
万方数据