An Establishment of Canard-Leading Edge Flap Scheduling Law Based on Experimental and Numerical Studies For the Aerodynamic Design of Canard Type Fighter Class Aircraft (카나드 형상 전투기급 항공기 공력설계를 위한 실험 및 수치해석적 카나드-앞전플랩 스케줄링 법칙 수립)
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- Journal of the Korean Society for Aeronautical & Space Sciences
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- v.35 no.7
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- pp.655-660
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- 2007