In order to eliminate the influence of static aeroelastics deformation and satisfy the flying characteristic requirement of aircraft, a new approach to the jig-shape elastic wing design problem is presented.
在研究机翼的静气动弹性规律的基础上,对机翼进行型架外形设计,使之在飞行中满足飞机设计气动外形的要求,并以一后掠机翼为算例,计算结果与有关文献相吻合。
