TBL and CBL Jet Injection Effects on Performance of SD7003 at Low Reynolds Number
Publish place: 17th Fluid Dynamics Conference
Publish Year: 1396
نوع سند: مقاله کنفرانسی
زبان: English
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شناسه ملی سند علمی:
CFD17_014
تاریخ نمایه سازی: 22 دی 1396
Abstract:
Blowing crossing the boundary layer have been widely implemented on the airfoils top surface to control the flow field. This technique has significant effects on the aerodynamic characteristics of the airfoil. This method was applied to SD7003 airfoil at Reynolds number of 60,000. The TBL (Tangential of Boundary Layer) and CBL (Cross to Boundary Layer) have been implemented. Results showed that application of active flow control method caused a reduction in flow separation zone which resulted in improvement of aerodynamic coefficients.
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Authors
Djavad Kamari
PhD Student of Amirkabir University of Technology
Mehran Tadjfar
Associate Professor of Amirkabir University of Technology