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RESEARCH ON SONIC FATIGUE CALCULATION AND TEST FOR AIRCRAFT PANEL
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作者 Ge Sen and Zhou Zhilun Aircraft Strength Research Institute (ASRI) 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 1991年第3期274-278,共5页
The sonic fatigue life of the aluminium rectangular panel was calculated using the concise method[1], and the sonic fatigue test was conducted on progressive wave tube (PWT) test facility. A comparison was made betwee... The sonic fatigue life of the aluminium rectangular panel was calculated using the concise method[1], and the sonic fatigue test was conducted on progressive wave tube (PWT) test facility. A comparison was made between the results of calculation and test, and it shows reasonable agreement between these two results. 展开更多
关键词 TEST RESEARCH ON SONIC fatigue CALCULATION AND TEST FOR aircraft PANEL
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