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机译:基于S.M.A.的机翼结构变形执行器系列:数值和实验研究
Aerospace Engineering Department(DIAS), University of Naples Federico II, Via Claudio 21, Naples- 80125, Italy;
Aerospace Engineering Department(DIAS), University of Naples Federico II, Via Claudio 21, Naples- 80125, Italy;
Aerospace Engineering Department(DIAS), University of Naples Federico II, Via Claudio 21, Naples- 80125, Italy;
Smart Structures Lab., The Italian Aerospace Research Centre (CIRA), Via Maiorise, Capua (CE) - 81043, Italy;
Smart Structures Lab., The Italian Aerospace Research Centre (CIRA), Via Maiorise, Capua (CE) - 81043, Italy;
Alenia Aeronautica S.p.a., Viale dell'Aeronautica snc, Pomigliano d'Arco (NA) - 80038, Italy;
smart structures; sma; morphing; hingeless flap; actuator;
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:DBD等离子作动器控制翼型边界层过渡的实验和数值研究
机译:加热致动双稳态复合材料层合板的数值与实验研究
机译:使用DBD等离子体致动器对边界层过渡控制的实验性和数值研究
机译:用于变形结构应用的纳米管巴克纸复合致动器的实验研究和建模。
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:DBD等离子驱动器对翼型边界层过渡控制的实验和数值研究
机译:柔性平面变形机翼分布式驱动系统的结构优化