unsteady aerodynamic loading meaning in Chinese

不稳定空气动力加载

Using local piston theory based on cfd to solve hypersonic unsteady aerodynamic loads , the hypersonic aerothermoelasticity is simulated in time domain
在时间域内实现了高超音速热气动弹性的仿真。
Using the engineering methods of supersonic and hypersonic flow or local piston theory developed in this paper to compute unsteady aerodynamic loads , and coupling structural equations , the supersonic or hypersonic aeroelasticity with a typical servo system under thermal environment is simulated in time - domain
运用超音速、高超音速气动力工程计算方法和本文发展的当地流活塞理论计算非定常气动力，耦合结构运动方程，实现了热环境中带有伺服机构的气动弹性的时域仿真。