Japan Aerospace Exploration Agency Wind Tunnel Technology Center, Institute of Space Technology and Aeronautics
出版者
宇宙航空研究開発機構
出版者（英）
Japan Aerospace Exploration Agency (JAXA)
雑誌名
宇宙航空研究開発機構特別資料: 第73回風洞研究会議論文集
雑誌名(英)
JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 73rd Meeting
巻
JAXA-SP-04-014
ページ
50 - 53
発行年
2005-03-30
抄録（英）
In a hypersonic shock tunnel, it is essential to extract aerodynamic force from oscillation-contaminated measurement. This paper proposes an oscillation identification technique method. The method identifies aerodynamic force by the parameter-matching technique. Verification test, applying this method to HB2 standard model, was satisfactory with completely consistent results.
振動同定除去法による衝撃風洞計測データからの空力6分力の推定
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