研究结果为地效飞行器的设计与优化提供理论依据。
The simulation results provide theoretical basis for the design and optimization on the crafts of wing in ground effect .
研究结果对地效飞行器的气动布局设计和研究有一定的指导和参考价值。
The present study provides theoretical basis for the design and research on configurations of WIG crafts.
得出的结论对于类似的地效飞行器或轻型飞机翼根连接设计具有一定参考价值。
And the conclusions are valuable for wing root joint designs such as those of ground effect aircraft or light airplane.
通过现有地效飞行器数据和资料的整理，研究其起飞重量与空机重量以及其他各项参数的统计关系。
By searching and sorting out the data of existing WIG, the statistic relationship of takeoff weight and empty weight as well as other parameters are studied.
分析了水面空气动力的成因、特点及其对地效飞行器的影响，提出了地效飞行器气动特性的预测方法。
Aerohydrodynamic characters and its effects on WIG are analyzed in this paper. Prediction methods of aerodynamics of WIG are presented.
关于地效飞行器的原理可以追溯到20世纪20年代——当德国物理学家卡尔*威尔斯贝格描述出地效原理的特点时。
The theory of ground-effect vehicles goes back to the 1920s, when Carl Wieselsberger, a German physicist, described how the ground effect works.
通过数据分析计算起飞重量和空机重量估算中的线性回归值，形成适用于各类地效飞行器的重量估算方法及其推荐经验系数。
Through data analysis and linear regression value calculation, the weight estimation methods and recommended experience factors which can be applied to every type of WIG are determined.
通过数据分析计算起飞重量和空机重量估算中的线性回归值，形成适用于各类地效飞行器的重量估算方法及其推荐经验系数。
Through data analysis and linear regression value calculation, the weight estimation methods and recommended experience factors which can be applied to every type of WIG are determined.
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