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机译:变形机翼和副翼系统的数值和实验过渡结果评估
Ecole Technol Super, Res Lab Act Control, Avion & AeroServoElast LARCASE, Montreal, PQ, Canada;
Ecole Technol Super, Res Lab Act Control, Avion & AeroServoElast LARCASE, Montreal, PQ, Canada;
Ecole Technol Super, Res Lab Act Control, Avion & AeroServoElast LARCASE, Montreal, PQ, Canada;
Ecole Technol Super, Res Lab Act Control, Avion & AeroServoElast LARCASE, Montreal, PQ, Canada;
Ecole Technol Super, Res Lab Act Control, Avion & AeroServoElast LARCASE, Montreal, PQ, Canada;
Ecole Technol Super, Res Lab Act Control, Avion & AeroServoElast LARCASE, Montreal, PQ, Canada;
Ecole Technol Super, Res Lab Act Control, Avion & AeroServoElast LARCASE, Montreal, PQ, Canada;
Ecole Technol Super, Res Lab Act Control, Avion & AeroServoElast LARCASE, Montreal, PQ, Canada;
NRC Aerosp, Aerodynam Lab, Ottawa, ON, Canada;
NRC Aerosp, Aerodynam Lab, Ottawa, ON, Canada;
Univ Naples Federico II, Ind Engn Dept, Aerosp Div, Naples, Italy;
Univ Naples Federico II, Ind Engn Dept, Aerosp Div, Naples, Italy;
Univ Naples Federico II, Ind Engn Dept, Aerosp Div, Naples, Italy;
Italian Aerosp Res Ctr CIRA, Adapt Struct Div, Capua, CE, Italy;
Italian Aerosp Res Ctr CIRA, Adapt Struct Div, Capua, CE, Italy;
Italian Aerosp Res Ctr CIRA, Adapt Struct Div, Capua, CE, Italy;
aerodynamics; Morphing Wing Tip; Genetic Optimization Algorithm; Flow Transition; Drag Coefficient Reduction; Wind Tunnel Tests; Morphing Aileron Classification Description: Aerodynamics; Aeroelasticity; Avionics and Systems; Computational Fluid Dynamics; Experimental Fluid Dynamics;
机译:全规模伺服驱动变形的数值和实验验证Aileron模型
机译:用于变形翼尖致动系统的模糊逻辑控制:设计,数值模拟和风洞实验测试
机译:飞机变形机翼模型中受控电致动系统的设计,数值模拟和实验测试
机译:装有常规副翼和副翼副翼的上翼变形机翼的数值和实验测试
机译:配备常规和变形副翼的翼尖结构优化方法的数值和实验验证=
机译:变形翼尖驱动系统的基于模糊逻辑的控制:设计数值模拟和风洞实验测试
机译:具有传统和变形翅片的翼尖结构的方法的数值和实验验证
机译:关于摆动翼 - 副翼系统气动衍生物测定的半实验方法的注记