The Low Reynolds Number Wing Aerodynamics and Micro Aerial Vehicles Development

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概要

• 論文の詳細を見る

• Micro Aerial Vehicle (MAV) has emerged as an attractive and significant research topic in aeronautical academia in last decade because of its profound applications and complicated aerodyanmics. This paper reports a summary of review about the MAV development and its low Reynolds number wing aerodynamic characteristics (such as instability and evolutional behavior) and vehicle design considerations made in past years in our lab. The most recent progress on optimization of single-winged and cascade-winged MAV design and flight tests is also discussed.

• 一般社団法人日本機械学会の論文
• 2004-09-04

著者

• HSIAO Fei-Bin

  Institute of Aeronautics and Astronautics, National Cheng Kung University

• Hsiao Fei-bin

  Institute Of Aeronautics And Astronautics National Cheng Kyung University

• Liu Yi-chung

  Institute Of Aeronautics And Astronautics National Cheng Kyung University

• Lin Chi-yu

  Institute Of Aeronautics And Astronautics National Cheng Kyung University

• Chen Tang-sen

  Department Of Aircraft Engineering Air Force Institute Of Technology

• Wang Di-Bao

  Institute of Aeronautics and Astronautics, national Cheng Kyung University

• Kao Hong

  Institute of Aeronautics and Astronautics, national Cheng Kyung University

• Payne Uon-Jien

  Department of Aircraft Engineering, Air Force Institute of Technology

• Kao Hong

  Institute Of Aeronautics And Astronautics National Cheng Kyung University

• Wang Di-bao

  Institute Of Aeronautics And Astronautics National Cheng Kyung University

• Payne Uon-jien

  Department Of Aircraft Engineering Air Force Institute Of Technology

• Hsiao Fei-bin

  Institute Of Aeronautics And Astronautics National Cheng Kung University

関連論文

• On Evolution of Flow Structure and Vortex Dynamics for Right-Angle and Sharp-Edged Orifice Plane Jet
• The Low Reynolds Number Wing Aerodynamics and Micro Aerial Vehicles Development
• On Evolution of Flow Structure and Vortex Dynamics for Right-Angle and Sharp-Edged Orifice Plane Jet

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