کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
8961063 | 1646462 | 2018 | 12 صفحه PDF | دانلود رایگان |
عنوان انگلیسی مقاله ISI
Detached Eddy-Simulation of Delta-Wing Post-Stall Flow Control
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کلمات کلیدی
موضوعات مرتبط
علوم انسانی و اجتماعی
علوم اجتماعی
تحقیقات ایمنی
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چکیده انگلیسی
Flow control can significantly improve the aerodynamic performances of delta wings. Yet, despite numerous studies of vortex control by leading-edge blowing still little research is focused on the post-stall regime and further consideration of the shear-layer reattachment through flow control is needed. This paper reports on the effects of unsteady jets on the global flow field at a very high angle of attack, α = 45â¦. For this, Detached-Eddy Simulations are conducted and validated with wind tunnel test results. The vortex shedding of the unperturbed delta-wing flow is investigated and compared to the perturbed case. It concludes that unsteady blowing energizes the shear layer and reorders at the same time the shedding mechanism eventually forming a big burst vortex structure that increases the lift significantly.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Transportation Research Procedia - Volume 29, 2018, Pages 46-57
Journal: Transportation Research Procedia - Volume 29, 2018, Pages 46-57
نویسندگان
Andrei Buzica, Manuel Biswanger, Christian Breitsamter,