节点文献
结冰对飞机动力学特性影响的分析方法及其进展
Analysis Methods and Its Development about Effect of Ice Accretion on Aircraft Flight Dynamics Characteristics
【摘要】 详细地介绍了常用的四种典型的结冰对飞机动力学特性影响的分析方法,即参量测算评估法、结冰影响参数法、神经网络气动建模法和动力学建模与仿真计算法,并讨论了各种分析方法的特点及其发展。
【Abstract】 The representative analysis techniques of icing effect on aircraft flight dynamics consist of a modified stepwise regression method, an neural network method,an icing severity parameter method and a flight dynamics modeling and simulation. In this paper, these representative analysis techniques and its peculiarity and development were described essentially.
【关键词】 飞机结冰;
动力学特性;
分析方法;
【Key words】 aircraft icing; flight dynamics characteristics; analysis method;
【Key words】 aircraft icing; flight dynamics characteristics; analysis method;
- 【文献出处】 飞行力学 ,Flight Dynamics , 编辑部邮箱 ,2004年04期
- 【分类号】V212
- 【被引频次】5
- 【下载频次】376