摘要
结合L8和N5A飞机的设计特点，对操纵面颤振规律、全复合材料垂尾颤振特性、风洞试验模型的动相似反设计等气动弹性技术作了研究。介绍了这些技术在L8和N5A飞机设计中的应用情况。
This paper researches on aeroelasticity technique such as flutter law of control surfaces, flutter behaviour of all-composite vertical tail and dynamic similarity updating design of wind-tunnel model in the light of L8 and N5A aircraft design characteristics. It introduces application of these technique in design of L8 and N5A aircraft.
出处
《洪都科技》
1995年第3期4-9,共6页
Hongdu Science and Technology
关键词
防颤振
复合材料
垂直尾翼
动相似反设计
飞机
Anti-flutter design All-composite vertical tail Dynamic similarity updating design
