National Aerospace Laboratory Airframe Division
National Aerospace Laboratory Airframe Division
Nagoya University
National Aerospace Laboratory Structural Mechanics Division
National Aerospace Laboratory Aerodynamics Division
National Aerospace Laboratory Aerodynamics Division
National Aerospace Laboratory Aerodynamics Division
National Aerospace Laboratory Aerodynamics Division
出版者
航空宇宙技術研究所
出版者（英）
National Aerospace Laboratory (NAL)
雑誌名
航空宇宙技術研究所資料
雑誌名(英)
Technical Memorandum of National Aerospace Laboratory
A new system of a flutter emergency stopper is developed for preventing catastrophic failure of wing models when they burst into flutter during supersonic blowdown in wind tunnel tests. This system is used in the tests of flutter boundary estimation of supersonic delta wings and is found to yield good results. The details of this system with some experimental results are described in this paper.
超音速フラッタ停止装置の開発
naltm00693.pdf
(1.29MB)
