The present work investigates the effects of two active boundary layer control methods – boundary layer suction and blowing- on drag reduction. This study has been carried out through wind tunnel testing and also computational fluid dynamics as follows: first, boundary layer suction on the rear slant of a generic car model –Ahmed model – is applied and its effects are studied. Then, an air flow with the same rate as suction flow is blown into the wake region of the model, simultaneously. Moreover, the effect of change in suction and blowing flow rate and also change in the suction and blowing area on aerodynamic drag reduction are investigated. The results show that application of the flow suction at the beginning of the rear slant of the model reduces the drag. Furthermore, the simultaneous application of suction at the rear slant and blowing at the wake region improves the performance of flow control in comparison with the case solely with suction. It is also observed that for a constant rate of blowing flow, bigger blowing area leads to more reduction in the drag. This work is carried out by M. Abbaspour under supervision of Dr. M. Jahanmiri at Shiraz University of Technology.
Les informations fournies dans la section « Synopsis » peuvent faire référence à une autre édition de ce titre.
The present work investigates the effects of two active boundary layer control methods – boundary layer suction and blowing- on drag reduction. This study has been carried out through wind tunnel testing and also computational fluid dynamics as follows: first, boundary layer suction on the rear slant of a generic car model –Ahmed model – is applied and its effects are studied. Then, an air flow with the same rate as suction flow is blown into the wake region of the model, simultaneously. Moreover, the effect of change in suction and blowing flow rate and also change in the suction and blowing area on aerodynamic drag reduction are investigated. The results show that application of the flow suction at the beginning of the rear slant of the model reduces the drag. Furthermore, the simultaneous application of suction at the rear slant and blowing at the wake region improves the performance of flow control in comparison with the case solely with suction. It is also observed that for a constant rate of blowing flow, bigger blowing area leads to more reduction in the drag. This work is carried out by M. Abbaspour under supervision of Dr. M. Jahanmiri at Shiraz University of Technology.
Les informations fournies dans la section « A propos du livre » peuvent faire référence à une autre édition de ce titre.
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Etat : New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Jahanmiri MohsenDr. Mohsen Jahanmiri is an associate professor in Aerospace Engineering.He has 27 years of academic and industry job experience. He has offered different courses and supervised many student projects in undergraduate a. N° de réf. du vendeur 5145184
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Taschenbuch. Etat : Neu. Drag reduction of a generic car model by active boundary layer control | Experimental and computational research on a car model for drag reduction by a novel active flow control method | Mohammad Abbaspour | Taschenbuch | Englisch | LAP Lambert Academic Publishing | EAN 9783659278204 | Verantwortliche Person für die EU: preigu GmbH & Co. KG, Lengericher Landstr. 19, 49078 Osnabrück, mail[at]preigu[dot]de | Anbieter: preigu. N° de réf. du vendeur 106200947
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Taschenbuch. Etat : Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - The present work investigates the effects of two active boundary layer control methods boundary layer suction and blowing- on drag reduction. This study has been carried out through wind tunnel testing and also computational fluid dynamics as follows: first, boundary layer suction on the rear slant of a generic car model Ahmed model is applied and its effects are studied. Then, an air flow with the same rate as suction flow is blown into the wake region of the model, simultaneously. Moreover, the effect of change in suction and blowing flow rate and also change in the suction and blowing area on aerodynamic drag reduction are investigated. The results show that application of the flow suction at the beginning of the rear slant of the model reduces the drag. Furthermore, the simultaneous application of suction at the rear slant and blowing at the wake region improves the performance of flow control in comparison with the case solely with suction. It is also observed that for a constant rate of blowing flow, bigger blowing area leads to more reduction in the drag. This work is carried out by M. Abbaspour under supervision of Dr. M. Jahanmiri at Shiraz University of Technology. N° de réf. du vendeur 9783659278204
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