A ducted fan aerial vehicle model using Magnus effect steering engine is proposed in this paper. This model utilizes a steering engine that comprises four cylinders that are symmetrically installed at the aft inside the duct. Interaction between the spinning cylinder surface and the duct jet flow causes the aerodynamic lift proportional to angular velocity of the cylinder. Therefore, operating range of the aerodynamic lift is guaranteed to be sufficiently wide. The efficiency of the proposed method is confirmed via numerical simulations on integrated flight dynamics developed in this study.
机构:
Hanbat Natl Univ, Dept Elect & Control Engn, Taejon 305719, South KoreaHanbat Natl Univ, Dept Elect & Control Engn, Taejon 305719, South Korea
Doh, Tae-Yong
Ryoo, Jung Rae
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Seoul Natl Univ Sci & Technol, Dept Elect & Informat Engn, Seoul 139743, South KoreaHanbat Natl Univ, Dept Elect & Control Engn, Taejon 305719, South Korea
Ryoo, Jung Rae
Chang, Dong Eui
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机构:
Univ Waterloo, Dept Appl Math, Waterloo, ON N2L 3G1, CanadaHanbat Natl Univ, Dept Elect & Control Engn, Taejon 305719, South Korea
机构:
Hanbat Natl Univ, Dept Elect & Control Engn, Taejon 305719, South KoreaHanbat Natl Univ, Dept Elect & Control Engn, Taejon 305719, South Korea
Doh, Tae-Yong
Ryoo, Jung Rae
论文数: 0引用数: 0
h-index: 0
机构:
Seoul Natl Univ Sci & Technol, Dept Elect & Informat Engn, Seoul 139743, South KoreaHanbat Natl Univ, Dept Elect & Control Engn, Taejon 305719, South Korea
Ryoo, Jung Rae
Chang, Dong Eui
论文数: 0引用数: 0
h-index: 0
机构:
Univ Waterloo, Dept Appl Math, Waterloo, ON N2L 3G1, CanadaHanbat Natl Univ, Dept Elect & Control Engn, Taejon 305719, South Korea