Gust load alleviation of a transport-type wing: Test and analysis

Y. Matsuzaki, T. Ueda, Yoshikazu Miyazawa, H. Matsushita

研究成果: Contribution to journalArticle

24 引用 (Scopus)

抜粋

The present paper describes experimental and analytical results of gust response of a 1/9-scale transport-type wing with a gust load alleviation system. A reduced-order feedback control filter is formed with the aid of a modified optimal control theory. The system using the feedback filter has been confirmed to be effective against both sinusoidal gust and atmospheric turbulence. Detailed comparison is made by taking into account the effect of location of the leading- and the trailing-edge control surfaces. In general, agreement between analysis and experiment is good.

元の言語英語
ページ(範囲)322-327
ページ数6
ジャーナルJournal of Aircraft
26
発行部数4
DOI
出版物ステータス出版済み - 1 1 1989

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

フィンガープリント Gust load alleviation of a transport-type wing: Test and analysis' の研究トピックを掘り下げます。これらはともに一意のフィンガープリントを構成します。

  • これを引用

    Matsuzaki, Y., Ueda, T., Miyazawa, Y., & Matsushita, H. (1989). Gust load alleviation of a transport-type wing: Test and analysis. Journal of Aircraft, 26(4), 322-327. https://doi.org/10.2514/3.45763