A forced oscillation system for damping derivative measurement in the T-38 trisonic wind tunnel

A forced oscillation system for the measurement of damping derivative due to an aircraft or missile model oscillatory motion in a wind tunnel test section is described. The forced oscillation technique is used for dynamic stability derivatives measurements in the T-38 wind tunnel. Two full-model app...

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Autors principals:	Samardžić Marija, Marinkovski Dragan, Ćurčić Dušan
Format:	Artigo
Idioma:	Inglês
Publicat:	Military Technical Institute, Belgrade 2018-01-01
Col·lecció:	Scientific Technical Review
Matèries:	aerodynamic derivatives stability derivatives forced oscillations oscillatory motion wind tunnel
Accés en línia:	https://scindeks-clanci.ceon.rs/data/pdf/1820-0206/2018/1820-02061803031S.pdf
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