机译:在致动器盘和风力涡轮机接近尾声时针对立体声PIV测量验证四个LES和涡旋模型
Delft Univ Technol, Dept Aerodynam Wind Energy Flight Performance & P, NL-2629 HS Delft, Netherlands;
Delft Univ Technol, Dept Aerodynam Wind Energy Flight Performance & P, NL-2629 HS Delft, Netherlands|Energy Res Ctr Netherlands ECN, NL-1755 ZG Petten, Netherlands;
Johns Hopkins Univ, Dept Mech Engn, Baltimore, MD 21218 USA|Johns Hopkins Univ, Ctr Environm & Appl Fluid Mech, Baltimore, MD 21218 USA|Univ Twente, Dept Phys, Mesa Inst, POB 217, NL-7500 AE Enschede, Netherlands|Univ Twente, JM Burgers Ctr Fluid Dynam, POB 217, NL-7500 AE Enschede, Netherlands;
Katholieke Univ Leuven, Dept Mech Engn, Celestijnenlaan 300 A, B-3001 Leuven, Belgium;
Delft Univ Technol, Dept Aerodynam Wind Energy Flight Performance & P, NL-2629 HS Delft, Netherlands;
Tech Univ Denmark, Dept Wind Energy, DK-2800 Lyngby, Denmark;
Johns Hopkins Univ, Dept Mech Engn, Baltimore, MD 21218 USA|Johns Hopkins Univ, Ctr Environm & Appl Fluid Mech, Baltimore, MD 21218 USA;
Delft Univ Technol, Dept Aerodynam Wind Energy Flight Performance & P, NL-2629 HS Delft, Netherlands;
Delft Univ Technol, Dept Aerodynam Wind Energy Flight Performance & P, NL-2629 HS Delft, Netherlands;
Katholieke Univ Leuven, Dept Mech Engn, Celestijnenlaan 300 A, B-3001 Leuven, Belgium;
Delft Univ Technol, Dept Aerodynam Wind Energy Flight Performance & P, NL-2629 HS Delft, Netherlands;
Energy Res Ctr Netherlands ECN, NL-1755 ZG Petten, Netherlands;
Horizontal axis wind turbine; Wind turbine wake; Large eddy simulation; Actuator disc; LES validation;
机译:使用风洞测量评估风机尾流的RANS /执行器盘模型
机译:使用改进的执行器圆盘模型和计算流体动力学模型,对Horns Rev离岸风电场中的水平轴风力涡轮机尾流进行建模
机译:关于理想扩散器增强风力涡轮机的潜力:借助于动量理论方法和自由唤醒环 - 涡旋执行器盘模型的研究
机译:浮动式海上风力涡轮机自由涡流分析的弯曲涡流细丝模型的开发,验证和应用
机译:为风力涡轮机应用开发时间精确的粘性拉格朗日涡流模型。
机译:使用执行器线技术模拟风力涡轮机尾流
机译:在致动器盘和风力涡轮机的近尾流中验证四个LEs和涡流模型以防止立体声pIV测量