机译:低速烟风洞中Busemann双翼飞机翼型的研究
Department of Aerospace Engineering, National Defense Academy, Yokosuka, Japan;
Department of Aerospace Engineering, National Defense Academy, Yokosuka, Japan;
Department of Aerospace Engineering, National Defense Academy, Yokosuka, Japan;
Department of Aerospace Engineering, National Defense Academy, Yokosuka, Japan;
Department of Aerospace Engineering, National Defense Academy, Yokosuka, Japan Technical Research and Development Institute, Ministry of Defense, Tachikawa, Japan;
biplane airfoil; high-lift device; aerodynamics; smoke wind tunnel; potential flows;
机译:低速风洞中机翼经过失速颤振的分叉行为
机译:湍流强度对低速风洞中风机性能和尾流恢复影响的实验研究
机译:风力机叶片翼型糖霜的风洞实验研究
机译:烟风洞中双翼机翼升力系数的初步研究
机译:流体动力学的设计研究:I-低速风洞的开发II-流体动力涡轮机排气管的流体动力学。
机译:翼型微型飞行器的机翼选择程序风洞实验和6DOF建模实现
机译:低速烟风隧道Busemann双翼型的研究
机译:JaXa硬壁低速风洞30p30N三元高扬程翼型板板噪声试验研究。