Box翼を持つマルチコプタの風洞試験

機関リポジトリ

書誌事項

タイトル別名
  • Wind Tunnel Testing of a Multicopter with Box Wing

抄録

流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2020オンライン (2020年9月28日-30日. 日本航空宇宙学会 : 宇宙航空研究開発機構(JAXA)オンライン会議)

Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2020 Online (September 28-30, 2020. The Japan Society for Aeronautical and Space Sciences : Japan Aerospace Exploration Agency (JAXA), Online meeting)

The aerodynamic characteristics including high angle of attack condition up to 95 degrees of the Box wing, in which the electric multicopter was surrounded by a duct like annular wing, were acquired by a wind tunnel test for use in a quiet Electric Vertical Take Off and Landing (eVTOL) aircraft. The Box wing is expected to be quieter by shielding the aerodynamic noise from the propeller. It was shown that the Box wing has a mild stall characteristic, the lift of the Box wing increases due to the effect of the propeller thrust, and that the current Box wing has no effect of improving the hovering ability.

形態: カラー図版あり

Physical characteristics: Original contains color illustrations

資料番号: AA2030013017

レポート番号: JAXA-SP-20-008

収録刊行物

詳細情報 詳細情報について

  • CRID
    1050574036237440512
  • NII論文ID
    120006954825
  • ISSN
    24332232
  • Web Site
    http://id.nii.ac.jp/1696/00047325/
  • 本文言語コード
    ja
  • 資料種別
    conference paper
  • データソース種別
    • IRDB
    • CiNii Articles

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