Flow Simulations with Ultra-Low Reynolds Numbers over Rigid and Flexible Airfoils Subject to Heaving and Flapping Motions
سال انتشار: 1396
نوع سند: مقاله ژورنالی
زبان: انگلیسی
مشاهده: 84
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شناسه ملی سند علمی:
JR_JAFM-10-2_025
تاریخ نمایه سازی: 3 بهمن 1400
چکیده مقاله:
Numerical simulations of flow patterns at ultra-low Reynolds numbers over rigid and flexible airfoils are presented, and the influence of flexibility on main aerodynamic properties are discussed. Typical unsteady flights like heaving and flapping are, in terms of Reynolds and Strouhal numbers, reduced frequencies and FSI (Fluid Structure Interaction) factor, are valuated. It has been found that for some flexibility levels, the aerodynamic forces and propulsive efficiency are enhanced if compared with a rigid airfoil. The mathematical technical approach used to solve the laminar-incompressible flow equations coupled with structural algorithms, is described.
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نویسندگان
D. Antonelli
Cordoba National University, Cordoba, Cordoba, ۵۰۰۰, Argentina
C. Sacco
Aeronautical University Institute, Cordoba, Cordoba, ۵۰۰۰, Argentina
J. Tamagno
Cordoba National University, Cordoba, Cordoba, ۵۰۰۰, Argentina