Stress Spectrum Algorithm Development for Fatigue Crack Growth Analysis and Experiment for Aircraft Wing Structure (항공기 주익구조물의 피로균열 진전 해석 및 실험을 위한 응력 스펙트럼 알고리즘 개발)
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- Transactions of the Korean Society of Mechanical Engineers A
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- v.39 no.12
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- pp.1281-1286
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- 2015