Research on sonic fatigue analysis method for typical civil aircraft material
With the application of new lightweight materials in structures of civil aircraft,evaluation of properties for new materials is required to carry out continually.So it is valuable to develop a feweffective engineering methods for properties characterization,which can decrease the research costs and periods.Sonic fatigue problem is one of the important terms of civil aircraft airworthiness examination.In this paper,a kind of engineering analysis method is employed to study the sonic response characteristics of the typical commercial skin-stiffener aircraft structure fabricated from aluminum alloys.In addition,the sonic response experiment for this structure is carried out,and the resonant frequency and root mean square (RMS) stress are measured.
Aircraft material aircraft structure sonic response resonant frequency root mean square (RMS) stress
Wang Yu Zhang Jiazhen Liang Jun Guo Dingwen
Beijing Aeronautical Science & Technology Research Institute of COMAC, Beijing 100083, China; Harbin Harbin Institute of Technology, Harbin 150001, China AVIC Aircraft Strength Research Institute, Xian 710065, China
国际会议
上海
英文
65-65
2012-10-19（万方平台首次上网日期，不代表论文的发表时间）