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.
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.
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.
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.
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.
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.
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.
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