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飞机设计中的颤振综合分析
引用本文:陈奎林.飞机设计中的颤振综合分析[J].南京航空航天大学学报,1999,31(6):686-690.
作者姓名:陈奎林
作者单位:洪都航空工业集团飞机设计研究所!南昌330024
摘    要:K8教练飞机设计中的颤振分析包括数值计算、风洞试验、地面试验和飞行试验等工作,这些工作是在飞机设计和制造的不同阶段进行的,且彼此相关密不可分。文中对每一项工作作了评述。指出若仅采用其中的某一项分析或试验表明飞机的颤特性尚有不充分之处。只有将各种分析和试验结果进行相互验证、比较和修正,并进行综合分析,才能得出该飞机颤振安全的正确结论。

关 键 词:颤振分析  风洞试验  飞行试验  综合分析  飞机设计

Synthetic Analysis of Flutter in Aircraft Design
Chen Kuilin,Research Institute of Aircraft DesignHongdu Aviation Industry Group Company,Nanchang.Synthetic Analysis of Flutter in Aircraft Design[J].Journal of Nanjing University of Aeronautics & Astronautics,1999,31(6):686-690.
Authors:Chen Kuilin  Research Institute of Aircraft DesignHongdu Aviation Industry Group Company  Nanchang
Institution:Chen Kuilin Research Institute of Aircraft DesignHongdu Aviation Industry Group Company Nanchang,330024
Abstract:In the design of K8 aircrafts, flutter analysis includes flutter computation, ground vibration test, wind tunnel test and flight flutter test. These jobs are made in the different stages of the aircraft design and the aircraft manufacture, and they are coherent with each other. In this paper, every job is discussed. It is not sufficient if flutter certification is based upon only analysis or test of the aircraft. After making systematic analysis for the results of all analyses or tests, the accurate conclusion of aircraft flutter characteristics can be received.
Keywords:flutter  wind tunnel tests  numerical method  flight testing  synthesize analysis
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