107 パワード・リフト機模型の後流測定

DOI

書誌事項

タイトル別名
  • Wake Measurement on Aircraft Model with USB Powered High Lift System

抄録

The aircraft employing the Upper Surface Blowing(USB) system as a poweredlift technology makes use of the energy of the engine exhoust to augument wing lift. The aircraft with the USB system achieves higher powered-lift by turning full downward the engine exhaust flow. To studying powered-lift characteristics, the wakes of the semi-span aircraft model with USB Powered high lift system were measured by a taversing wake rake with 5-pitot tube in NAL 2×2m Gust Wind Tunnel.<BR>In this report, the characteristics for the wake having different turning angle of exhaust flow are described.

収録刊行物

詳細情報 詳細情報について

  • CRID
    1390001204619366400
  • NII論文ID
    130003442959
  • DOI
    10.3154/jvs.13.supplement2_35
  • ISSN
    1884037X
    09164731
  • 本文言語コード
    ja
  • データソース種別
    • JaLC
    • Crossref
    • CiNii Articles
  • 抄録ライセンスフラグ
    使用不可

問題の指摘

ページトップへ