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Composite wing flutter speed and frequency due to variable control surface deflection in low speed wind tunnel

Flutter is a dynamic instability problem represents the interaction among structural, aerodynamic, elastic and inertial forces and occurred when the energy is continuously transformed by the surrounding fluids to a flying structure in the form of kinetic energy. The study was conducted to investigat...

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書誌詳細
主要な著者:	Mahzan, M. I., Muhamad, S., Abdul Aziz, S., Mat Ali, M. S.
フォーマット:	Conference or Workshop Item
出版事項:	2013
主題:	T Technology
オンライン･アクセス:	http://eprints.utm.my/id/eprint/50954/ http://dx.doi.org/10.4028/www.scientific.net/AMM.390.3
タグ:	タグ追加タグなし, このレコードへの初めてのタグを付けませんか!

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