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NTIS 바로가기한국항공우주학회지 = Journal of the Korean Society for Aeronautical & Space Sciences, v.50 no.2, 2022년, pp.75 - 82
전민혁 (Chungnam National University) , 공승택 (Chungnam National University) , 조현준 (Chungnam National University) , 김인걸 (Chungnam National University) , 박재상 (Chungnam National University) , 유준태 (Korea Aerospace Research Institute) , 윤영하 (Korea Aerospace Research Institute)
Nondestructive method to predict buckling load for the propellant tank of launch vehicle should be evaluated. Vibration correlation technique can predict the global buckling load of unstiffened cylindrical structure with geometric initial imperfection using correlation of natural frequency and compr...
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