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A theoretical analysis of the effect of aileron inertia and hinge moment on the maximum rolling acceleration of airplanes in abrupt aileron rolls

机译：副翼惯性和铰链力矩对突然副翼辊飞机最大滚动加速度影响的理论分析

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作者
O'Sullivan, William J;
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年度 1942
页码 1-18
总页数 18
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AILERONS - HINGE MOMENTS; MOMENTS OF INERTIA; ROLLING MOMENTS; ACCELERATIONS IN ROLL; AILERONS - DEFLECTION;

机译：aILERONs - HINGE mOmENTs;惯性的时刻;滚动的时刻;滚动加速度; aILERONs - DEFLECTION;

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1. Aileron size and location to minimise induced drag during rolling-moment production at zero rolling rate [J] . Brincklow J. R., Hunsaker D. F. The Aeronautical Journal . 2021,第1287期

机译：Aileron大小和位置，以最大限度地减少零轧率下滚动力矩生产中的诱导阻力
2. Investigation of the Three-Dimensional Hinge Moment Characteristics Generated by the ONERA-M6 Wing with an Aileron [J] . G. Q. Zhang, S. C. M. Yu, A. Chien Advances in Mechanical Engineering . 2013,第Pta5期

机译：带有副翼的ONERA-M6机翼产生的三维铰链矩特性的研究
3. DECATHLON AILERON HINGE SUPPORT CRACKING RESOLVED [J] . The aviation consumer . 2017,第9期

机译：十项全能AILERON铰链支持解决
4. NUMERICAL INVESTIGATION OF AN AILERON HINGE MOMENTS AND EFFECTIVENESS ON A HIGH LIFT WING AIRFOIL [C] . K.A.Makarov, A.A.Pavlenko Congress of the International Council of the Aeronautical Sciences;International Council of the Aeronautical Sciences . 2014

机译：高升力机翼翼型铰链弯矩的数值研究及效果
5. Optimization of Aileron Spanwise Size and Shape to Minimize Induced Drag in Roll with Correlating Adverse Yaw [D] . ?Brincklow, Joshua R. 2020

机译：翼展方向副翼大小和形状的优化，以尽量减少诱导阻力在摇船进行相关不良偏航
6. Optimization design of a novel X-type six-high rolling mill based on maximum roll system stiffness [O] . Liping Wang, Qingyu Zhu, Hongyang Zhao 2020

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7. Numerical considerations relative to simulation of aileron-ruder controls in the roll-yaw motion [O] . Claudia Alice STATE 2010

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A theoretical analysis of the effect of aileron inertia and hinge moment on the maximum rolling acceleration of airplanes in abrupt aileron rolls

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