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机译:微型飞机应用中摆线转子概念的性能
Alfred Gessow Rotorcraft Center, Department of Aerospace Engineering Glenn L. Martin Institute of Technology, University of Maryland, College Park, MD;
Alfred Gessow Rotorcraft Center, Department of Aerospace Engineering Glenn L. Martin Institute of Technology, University of Maryland, College Park, MD;
Alfred Gessow Rotorcraft Center, Department of Aerospace Engineering Glenn L. Martin Institute of Technology, University of Maryland, College Park, MD;
Alfred Gessow Rotorcraft Center, Department of Aerospace Engineering Glenn L. Martin Institute of Technology, University of Maryland, College Park, MD;
A: rectangular projected area, (b × D), m~2; b: blade span, m; C_p: power coefficient, P/ρA(ΩR)~3; C_T: thrust coefficient, T_(Res)/ρA(ΩR)~2; C_d: drag coefficient; et al;
机译:开发用于微型飞行器的中尺度摆线旋翼飞机
机译:桨距不对称运动学对微型航空航天摆线转子正向飞行性能的影响
机译:流量曲率对微型空车摆线转子正向飞行性能的影响
机译:悬停微型飞行器摆线转子概念的实验研究
机译:对微型飞行器应用中摆线转子概念的基本了解。
机译:物理绩效措施对常规防护概念进行常规糖尿病的应用:握力的基本数据步态速度定时椅子站速度稳定平衡和膝关节延长力
机译:提高微型空车摆线转子的空气动力学性能:一种实验方法
机译:用于海军应用的智能车辆。第二部分。相关技术和绩效评估。海洋表面军事用智能车概念研究工作中期报告