aircraft testing; laminar flow; wind tunnels; pressure measurement; laser velocimetry; boundary layers; finite element analysis; flow measurement; aerodynamics; infrared imaging; flow simulation; flow control; 2D profile testing; Reynolds number; cryogenic wind tunnel Cologne; aircraft; 2D profile measuring technique; wind tunnels; servomotor; synchronized motor drive system; boundary layer control; thermal load; aerodynamic load; motor drive system; boundary conditions; pressure measurement; infrared thermograph; laser velocimetry; numerical methods; wind tunnel wall effect; wall correction method; windmills; laminar flow;
机译:雷诺数对低温风洞科隆DNW-KKK风力涡轮机轮廓影响的实验研究
机译:在两个不同的风隧道中进行风力涡轮机翼型上的高雷诺数2D试验的分析
机译:雷诺数对243 m高太阳塔在风洞试验中的风致响应的影响
机译:低雷诺数在低温隧道古龙水中的高雷诺数推进
机译:用于水平轴风力涡轮机转子测试的风洞测试设备的开发
机译:在山墙屋顶建筑物上进行风压分布的风洞测试
机译:用于高雷诺数测试的低温风洞
机译:低温风洞科隆