Forced oscillations of airfoil flows

The effect of background flow oscillations on a transonic airfoil (NACA 0012) flow was investigated experimentally. The oscillations were generated by means of a rotating plate placed downstream of the airfoil. Owing to the expansion and compression waves generated at the plate, the flow over the ai...

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Bibliographische Detailangaben

Veröffentlicht in:	Experiments in fluids 1996-10, Vol.21 (6), p.457-464
Hauptverfasser:	SZUMOWSKI, A. P, MEIER, G. E. A
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Applied fluid mechanics Exact sciences and technology Fluid dynamics Fundamental areas of phenomenology (including applications) Physics
Online-Zugang:	Volltext
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