Improvement in Aerodynamic Characteristics of a Paraglider Wing Canopy

• MASHUD Mohammad

  Department of Aerospace Engineering, Nagoya University

• UMEMURA Akira

  Department of Aerospace Engineering, Nagoya University

抄録

To determine the parameters which can improve the overall performance of a paraglider wing canopy, we have been investigating the fundamental aerodynamic characteristics of an inflatable cell model which is designed to represent the dynamic behaviors of each cell comprising the wing canopy. This paper describes the results of a series of wind tunnel experiments. It is shown that significant drag reduction can be achieved by adopting an appropriately designed shape for the soft cloth comprising the upper surface. A trade-off relationship between the aerodynamic quality (characterized by the lift-to-drag ratio) and structural strength (characterized by the internal air pressure coefficient) of the canopy is also examined in detail.

収録刊行物

• TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

  TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 49 (165), 154-161, 2006

  一般社団法人 日本航空宇宙学会

キーワード

• Paraglider
• Wind Tunnel Experiment
• Inflatable Cell Model
• Aerodynamic Characteristics

詳細情報

• CRID: 1390282679055869824
• NII論文ID: 10018428177
• NII書誌ID: AA0086707X
• DOI: 10.2322/tjsass.49.154
• ISSN: 21894205
• ISSN: 05493811
• NDL書誌ID: 8537227
• Web Site: https://ndlsearch.ndl.go.jp/books/R000000004-I8537227
• Web Site: https://www.jstage.jst.go.jp/article/tjsass/49/165/49_165_154/_pdf
• 本文言語コード: en
• データソース種別:
  • JaLC
  • NDL
  • Crossref
  • CiNii Articles
• 抄録ライセンスフラグ: 使用不可