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Détail de l'auteur
Auteur Noor A. Ahmed
Documents disponibles écrits par cet auteur
Affiner la rechercheParametric study of dynamic stall flow field with synthetic jet actuation / Joshua Yen in Transactions of the ASME . Journal of fluids engineering, Vol. 134 N° 7 (Juillet 2012)
[article]
in Transactions of the ASME . Journal of fluids engineering > Vol. 134 N° 7 (Juillet 2012) . - 08 p.
Titre : Parametric study of dynamic stall flow field with synthetic jet actuation Type de document : texte imprimé Auteurs : Joshua Yen, Auteur ; Noor A. Ahmed, Auteur Année de publication : 2012 Article en page(s) : 08 p. Note générale : fluids engineering Langues : Anglais (eng) Mots-clés : dynamic stall; unsteady flow; synthetic jet; spectral analysis Index. décimale : 620.1 Essais des matériaux. Défauts des matériaux. Protection des matériaux Résumé : A parametric study of the interaction between dynamic stall and a zero-net mass flux synthetic jet installed on a wing was investigated by identifying the dominant frequencies in the resulting flow field using spectral analysis. The instantaneous pressure distribution around an NACA 0020 wing was recorded by performing static and dynamic experiments using an open jet subsonic wind tunnel located at the aerodynamics laboratory of the University of New South Wales. The results obtained provided valuable insight into the interaction process. The oscillation frequency and its harmonics were identified in baseline dynamic experiments, as well as the jet frequency and offset frequencies with synthetic jet actuation. The offset frequencies, similar to beat frequencies, were found to be a dynamic effect and represented the complex and nonlinear interaction between dynamic stall and the synthetic jet. The study suggests that low amplitude synthetic jet actuation would be an effective method in enhancing the overall aerodynamic efficiency of the wing. This confirmed the viability of utilizing synthetic jets in dynamic stall control. DEWEY : 620.1 ISSN : 0098-2202 En ligne : http://asmedl.org/getabs/servlet/GetabsServlet?prog=normal&id=JFEGA4000134000007 [...] [article] Parametric study of dynamic stall flow field with synthetic jet actuation [texte imprimé] / Joshua Yen, Auteur ; Noor A. Ahmed, Auteur . - 2012 . - 08 p.
fluids engineering
Langues : Anglais (eng)
in Transactions of the ASME . Journal of fluids engineering > Vol. 134 N° 7 (Juillet 2012) . - 08 p.
Mots-clés : dynamic stall; unsteady flow; synthetic jet; spectral analysis Index. décimale : 620.1 Essais des matériaux. Défauts des matériaux. Protection des matériaux Résumé : A parametric study of the interaction between dynamic stall and a zero-net mass flux synthetic jet installed on a wing was investigated by identifying the dominant frequencies in the resulting flow field using spectral analysis. The instantaneous pressure distribution around an NACA 0020 wing was recorded by performing static and dynamic experiments using an open jet subsonic wind tunnel located at the aerodynamics laboratory of the University of New South Wales. The results obtained provided valuable insight into the interaction process. The oscillation frequency and its harmonics were identified in baseline dynamic experiments, as well as the jet frequency and offset frequencies with synthetic jet actuation. The offset frequencies, similar to beat frequencies, were found to be a dynamic effect and represented the complex and nonlinear interaction between dynamic stall and the synthetic jet. The study suggests that low amplitude synthetic jet actuation would be an effective method in enhancing the overall aerodynamic efficiency of the wing. This confirmed the viability of utilizing synthetic jets in dynamic stall control. DEWEY : 620.1 ISSN : 0098-2202 En ligne : http://asmedl.org/getabs/servlet/GetabsServlet?prog=normal&id=JFEGA4000134000007 [...]