Investigation of the Intake Stability of Bank-to-Turn Supersonic Missile under Sideslip Angle Based on CFD Analysis (CFD 해석 기반 종축기동 초음속 비행체의 옆미끄럼각에 따른 흡입구 안정성 분석)
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- Journal of the Korean Society of Propulsion Engineers
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- v.18 no.3
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- pp.8-16
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- 2014