机译:气动弹性风洞试验用于气动不确定性模型验证
Beijing University of Aeronautics and Astronautics, 100191 Beijing, People's Republic of China,School of Aeronautic Science and Engineering;
Beijing University of Aeronautics and Astronautics, 100191 Beijing, People's Republic of China,School of Aeronautic Science and Engineering;
Beijing University of Aeronautics and Astronautics, 100191 Beijing, People's Republic of China,Aeronautic Science and Engineering;
Shanghai Aircraft Design and Research Institute, 201210 Shanghai, People's Republic of China,Engineer, Commercial Aircraft Corporation of China, Ltd;
机译:翅片执行器系统的气动弹性半物理模拟和风洞测试验证
机译:在全桥气动弹性模型上进行风洞测试的调谐质量阻尼器建模
机译:在全桥气动弹性模型上进行风洞测试的调谐质量阻尼器建模
机译:气动弹性风洞试验用于气动不确定性模型验证
机译:超音速充气气动减速器的气动弹性分析和测试。
机译:空气动力学模型的绝对观点用于桥面板的空气弹性分析
机译:估算风洞模型静态空气弹性变形的简单空气动力学建模
机译:气动弹性直升机旋翼模型的风洞试验,