| 单旋翼式直升机气动布局的几个问题 |
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| 引用本文： | 郭才根,徐国华.单旋翼式直升机气动布局的几个问题[J].南京航空航天大学学报,1996,28(3):309-314. |
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| 作者姓名： | 郭才根 徐国华 |
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| 作者单位： | 南京航空航天大学飞行器系 |
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| 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益的一些基本方法。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，该方法是十分有效的。
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| 关 键 词： | 直升机 旋翼 总体设计 气动布局 |
Some Problems on Aerodynamic Configuration for the Single Rotor Helicopter |
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| Abstract: | 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. |
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| Keywords: | helicopters rotors helicopter design preliminary design of the helicopter design of aerodynamic configuration for the helicopter |
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