지원사업
학술연구/단체지원/교육 등 연구자 활동을 지속하도록 DBpia가 지원하고 있어요.
커뮤니티
연구자들이 자신의 연구와 전문성을 널리 알리고, 새로운 협력의 기회를 만들 수 있는 네트워킹 공간이에요.
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초록· 키워드
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The free-wing tilt-body aircraft is researched in the flight performance characteristics such as short take-off and landing capability, and reduced sensitivity to gust and center of gravity (CG) change. Due to the main wing separating from the fuselage, the high tiltable empennage, and the stub-wing strongly influencing from the propeller wake, the resulting vehicle aerodynamics and flight dynamics are quite different from those of a conventional fixed-wing aircraft. Using the governing flight dynamics model was studied previously, all of speed and body tilt angle is simulated to determine the flight envelope by a non-linear 3-DOF flight simulation analysis. Though flight performance and trimmability are studied, the flight model of free-wing tilt-body aircraft is to reduce the hidden risk and to achieve the successful flight test. It is analyzed the flight characteristics that distinguishes free-wing tilt-body aircraft from the conventional aircraft.
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등록된 정보가 없습니다.
참고문헌 (9)
참고문헌 신청
Zuck, D.R / 1949 / U.S. Patent No. 2,347,230
Spratt, C.G. / U.S. Patent No. 2,623,712
Schmittle, H.J. / 1986 / U.S. Patent No. 4,596,368
Chen, W. / 1995 / A Wind Tunnel Test of a Tilt-body Freewing Aircraft Including Thrust Effects / AIAA-95-1902, AIAA Applied Aerodynamics Conference
Ro.K / 2007 / Aerodynamic Characteristics of a Free-Wing Tilt-Body Unmanned Aerial Vehicle / Journal of Aircraft 44(3):1619~1629
Spratt, C.G. / U.S. Patent No. 2,623,712
Schmittle, H.J. / 1986 / U.S. Patent No. 4,596,368
Chen, W. / 1995 / A Wind Tunnel Test of a Tilt-body Freewing Aircraft Including Thrust Effects / AIAA-95-1902, AIAA Applied Aerodynamics Conference
Ro.K / 2007 / Aerodynamic Characteristics of a Free-Wing Tilt-Body Unmanned Aerial Vehicle / Journal of Aircraft 44(3):1619~1629
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