1枚の翼で構成された尾翼の操舵特性 Aerodynamic Characteristics of a Single Wing Tail System

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抄録

Aerodynamic characteristics of a tail system which consists of a single wing was examined experimentally. Although many conventional airplanes are equipped with one or more vertical tail(s) and a pair of horizontal tail for longitudinal and directional control, respectively, a wind tunnel experiment revealed that an appropriately configured single wing can control pitch and yaw of an airplane. The windtunnel test was performed on a model which consists of a main wing and a single wing tail. Aerodynamic forces were measured by a force balance and oil-flow visualization was performed as well. In the windtunnel test, two different steering methods of a single wing tail system were examined and both of them were shown to work compatibly.

収録刊行物

  • 日本航空宇宙学会論文集 = Journal of the Japan Society for Aeronautical and Space Sciences

    日本航空宇宙学会論文集 = Journal of the Japan Society for Aeronautical and Space Sciences 56(648), 22-28, 2008-01-05

    一般社団法人 日本航空宇宙学会

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各種コード

  • NII論文ID(NAID)
    10021152804
  • NII書誌ID(NCID)
    AA11307372
  • 本文言語コード
    JPN
  • 資料種別
    ART
  • ISSN
    13446460
  • NDL 記事登録ID
    9351671
  • NDL 雑誌分類
    ZN25(科学技術--運輸工学--航空機・ロケット)
  • NDL 請求記号
    Z74-B503
  • データ提供元
    CJP書誌  NDL  J-STAGE 
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