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机译:用于减少攻击性攻角,摊位和失去后条件下的机翼自噪声的前沿锯齿
Univ Southampton Inst Sound &
Vibrat Res Southampton SO17 1BJ Hants England;
Univ Southampton Inst Sound &
Vibrat Res Southampton SO17 1BJ Hants England;
Univ Nottingham Fac Engn Nottingham England;
Univ Southampton Aerodynam &
Flight Mech Res Grp Southampton Hants England;
Univ Southampton Inst Sound &
Vibrat Res Southampton SO17 1BJ Hants England;
Univ Nottingham Fac Engn Nottingham England;
Univ Southampton Aerodynam &
Flight Mech Res Grp Southampton Hants England;
Brunel Univ Dept Mech Aerosp &
Civil Engn Uxbridge Middx England;
Brunel Univ Dept Mech Aerosp &
Civil Engn Uxbridge Middx England;
Technion Israel Inst Technol Haifa Israel;
City Univ London Sch Math Comp Sci &
Engn London England;
City Univ London Sch Math Comp Sci &
Engn London England;
City Univ London Sch Math Comp Sci &
Engn London England;
Stall noise; leading edge serrations; noise reductions; aerofoil self-noise;
机译:通过多波长前缘锯齿的空气湍流相互作用噪声减少
机译:通过双波长前缘锯齿驾驶机架宽带噪声减少:新的控制概念
机译:薄机井的前缘噪声和空气动力学对直线和弯曲的锯齿
机译:用于减少机翼分离自噪声的前沿锯齿
机译:接近前缘齐平安装的迎角传感器的设计,安装和测试。
机译:PELskin项目第五部分:使用自激活可展开襟翼以大迎角控制翼型周围的流动
机译:前沿锯齿,用于减少空气滤器自噪声,处于低攻角,摊位和失踪后的条件
机译:前翼楔对翼型上表面和前缘气动效应的实验研究,重点是高角度攻击