摘要
通过对某型号直升机气动布局设计，介绍了在直升机总体设计中选择直升机气动外形、平尾和尾桨的参数及位置的一些基本方法。文中还介绍了对应的风洞试验结果，并将其与理论计算结果进行对比。实例应用证明。
Taking a certain model of the helicopter as an example,a method for selecting the aerodynamic shape of a fuselage ,the parameters and locations of a horizontal stabilizer and a tail rotor in the preliminary design is presented.The comparison of a calculation using the method presented in the paper with corresponding wind tunnel test results indicates that the method presented is quite effective.
出处
《南京航空航天大学学报》
CAS
CSCD
1996年第3期309-314,共6页
Journal of Nanjing University of Aeronautics & Astronautics
关键词
直升机
旋翼
总体设计
气动布局
helicopters
rotors
helicopter design
preliminary design of the helicopter
design of aerodynamic configuration for the helicopter
