介绍了基于地效翼船空间运动方程的自控参数优化方法。
A method based on the space motion equation of Wing-In-Ground-Effect Ship (WIG Ship) for optimization of automatic control parameters is introduced.
这种地效翼船水平尾翼，升力大、面积小、生产成本低。
The horizontal tail wing of the wing-in-ground effect craft has the advantages of great ascensional force, small area and low production cost.
利用地效翼卸载技术实现海上运输平台高超临界航行，是一种全新的概念。
This paper presented a new theory of high supercritical planning by wing-in-ground effect unloading technology.
在军事上，地效翼船无论是作为实施袭击的平台还是登陆作战的工具，保持低空飞行状态都是必须的；
Either to be a platform for originating an attack to the enemy or to be a vehicle for landing force, the WIG vehicle must fly with low altitude in martial action.
同时，除相对飞高外，翼剖面的厚度和拱度对地效翼的气动力特性也有重要影响。进而，作者对应用CFD分析或辅助地效翼气动力风洞试验进行了探讨。
The calculation results also showed that besides the relative ground clearance, the ratios of thickness and camber of wing profile have significant influence on the aerodynamics of WIGs.
本研究以隐式差分方法求解不可压RANS方程，对二维地效应翼的性能及周围流场进行数值模拟。
The performance and flows of 2-D Wing-In-Ground Effect are numerically simulated by solving RANS equations using an implicit finite difference method.
本研究以隐式差分方法求解不可压RANS方程，对二维地效应翼的性能及周围流场进行数值模拟。
The viscous flow between the wing-tip and the wall is simulated by solving the RANS equations of incompressible fluid.
本研究以隐式差分方法求解不可压RANS方程，对二维地效应翼的性能及周围流场进行数值模拟。
The viscous flow between the wing-tip and the wall is simulated by solving the RANS equations of incompressible fluid.
应用推荐