机译:一种新的优化方法,可改善厚型风力涡轮机机翼的整体性能
Chinese Acad Sci, Inst Engn Thermophys, Beijing 100190, Peoples R China|Chinese Acad Sci, Key Lab Wind Energy Utilizat, Beijing 100190, Peoples R China|Natl Res & Dev Ctr Wind Turbine Blade, Beijing 100190, Peoples R China;
Chinese Acad Sci, Inst Engn Thermophys, Beijing 100190, Peoples R China|Chinese Acad Sci, Key Lab Wind Energy Utilizat, Beijing 100190, Peoples R China|Natl Res & Dev Ctr Wind Turbine Blade, Beijing 100190, Peoples R China;
Chinese Acad Sci, Inst Engn Thermophys, Beijing 100190, Peoples R China|Chinese Acad Sci, Key Lab Wind Energy Utilizat, Beijing 100190, Peoples R China|Natl Res & Dev Ctr Wind Turbine Blade, Beijing 100190, Peoples R China;
Chinese Acad Sci, Inst Engn Thermophys, Beijing 100190, Peoples R China|Chinese Acad Sci, Key Lab Wind Energy Utilizat, Beijing 100190, Peoples R China|Natl Res & Dev Ctr Wind Turbine Blade, Beijing 100190, Peoples R China;
Horizontal axis wind turbine; Thick airfoil; Overall aerodynamic performance; Evaluating parameters; Numerical optimization; Mid span of blade;
机译:翼型优化,以中等速比提高高强度垂直轴风力发电机的动力性能
机译:利用遗传算法优化厚风涡轮机翼型
机译:非常厚的风轮机翼CAS-W1-450的不稳定空气动力学性能
机译:风力涡轮机厚翼型的混合优化
机译:研究新型湍流模型并使用前沿槽改善机翼和风力涡轮机的空气动力学性能。
机译:使用多流管模型和遗传算法优化机翼以提高垂直轴风力发电机的动力性能
机译:改善双等式涡流湍流模型,以预测厚风力涡轮机翼型的空气动力学性能