A Study on Structural Analysis for Aircraft Gas Turbine Rotor Disks Using the Axisymmetric Boundary Integral Equation Method (축대칭 경계적분법에 의한 항공기 가스터빈 로터디스크 구조해석에 관한 연구)
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- Transactions of the Korean Society of Mechanical Engineers A
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- v.20 no.8
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- pp.2524-2539
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- 1996