丸い前縁を有するボルテックス・フラップ付きデルタ翼の低速空力特性について

• RINOIE Kenichi

  東京大学

Bibliographic Information

Other Title

• マルイ ゼンエン オ ユウスル ボルテックス フラップ ツキ デルタヨク ノ テイソク クウリキ トクセイ ニ ツイテ

Abstract

Low speed wind tunnel measurements were done on 50°and 60°delta wings with rounded leading-edge vortexflaps in order to assess the benefits of the rounded leading-edge vortex flaps. Deflecting the rounded leading-edge vortexflaps improves the lift/ drag ratio at relatively higher lift coefficients, when compared with the sharp edged vortex flaps.

Journal

• Aeronautical and Space Sciences Japan

  Aeronautical and Space Sciences Japan 48 (560), 512-515, 2000-09-05

  THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

Keywords

• Vortex Flap
• Rounded Leading-Edge
• Delta Wing

Details

• CRID: 1390845713060460928
• NII Article ID: 10004623457
• NII Book ID: AN00189072
• DOI: 10.14822/kjsass.48.560_512
• ISSN: 24241369
• ISSN: 00214663
• NDL BIB ID: 5485389
• Web Site: https://ndlsearch.ndl.go.jp/books/R000000004-I5485389
• Text Lang: ja
• Data Source:
  • JaLC
  • NDL
  • CiNii Articles
• Abstract License Flag: Disallowed