A modified Beddoes-Leishman dynamic stall model for wind turbine applications

Dynamic stall is phenomenon that plays a role in many applications such as helicopter or wind turbine aerodynamics. Proper modelling of unsteady lift, drag, and pitching moment characteristics of an airfoil undergoing dynamic stall can help to give more accurate performance predictions, but has turn...

وصف كامل

محفوظ في:
التفاصيل البيبلوغرافية
المؤلف الرئيسي: Reinecke, Arne
مؤلفون آخرون: Chua Leok Poh
التنسيق: Theses and Dissertations
اللغة:English
منشور في: 2018
الموضوعات:
الوصول للمادة أونلاين:http://hdl.handle.net/10356/74184
الوسوم: إضافة وسم
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المؤسسة: Nanyang Technological University
اللغة: English
الوصف
الملخص:Dynamic stall is phenomenon that plays a role in many applications such as helicopter or wind turbine aerodynamics. Proper modelling of unsteady lift, drag, and pitching moment characteristics of an airfoil undergoing dynamic stall can help to give more accurate performance predictions, but has turned out to be extremely challenging. The so-called Beddoes-Leishman models – based on indicial formulation with semi-empirical parameters – are considered current state-of-the-art and are incorporated in Blade Element Momentum as well as Vortex Wake Methods in codes for aerodynamic wind turbine analysis. These models contain empirical parameters and time constants that need to be determined manually by comparison to experimental data in a tedious, ’trial & error’ fashion. This thesis investigates the uses of numerical techniques to find optimal values for these parameters. An Evolutionary Strategy is employed optimizing the parameter set and thus, coming up with a parameter set that gives similar, if not better match to the experimental data than default values.