Aerodynamic Characteristics of the Blended-Wing-Body for the Position and Aspect Ratio of the Inlet and Outlet of an Embedded Distributed Propulsion System (Embedded Type 분산 추진 장치의 입·출구 형상 및 위치 변화에 따른 융합익기의 공력해석)
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- Journal of the Korean Society for Aeronautical & Space Sciences
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- v.40 no.6
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- pp.467-474
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- 2012