دانلود پایان نامه انگلیسی دربارۀ ایرودینامیک توربین بادی
This thesis hence aims to improve our understanding of rotor aerodynamics
in yaw using wind tunnel experiments. Its concrete objectives are:
quantify the effects of experimentally observed yaw misalignment on
rotor inflow and blade loads
• identify the aerodynamic mechanisms governing the effects of yaw misalignment
on rotor inflow and blade loads
• assess the validity of semi-empirical submodels, used to patch BEMtheory;
the Glauert momentum equation for yaw, induction non-uniformity
corrections in yaw, airfoil dynamic stall models.