机译:先进隐形飞机在水隧道中的静态和动态空气特性测试
Dean of R&D Division, Chung Hwa University of Medical Technology, Tainan, Taiwan, ROC;
Department of Mechanical Engineering, National Chung-Hsing University, Taichung, Taiwan, ROC;
Department of Mechanical Engineering, National Chung-Hsing University, Taichung, Taiwan, ROC;
Aeronautical Systems Research Division, Chung-Shan Institute of Science and Technology, Taichung, Taiwan, ROC;
Department of Mechanical Engineering, National Chung-Hsing University, Taichung, Taiwan, ROC;
X-45A/stealth; longitudinal stability; reduced frequency; hysteresis behavior;
机译:滑水道中翼翼飞行器的静态和动态空气特性测试
机译:计算流体动力学和风洞测试在飞机开发中的相对作用
机译:跨音速动力学隧道气弹性测试,以支持飞机开发
机译:从F-16XL飞机的动态水隧道试验获得的渐进式空气动力学模型识别
机译:使用通过风洞测试验证的计算流体动力学对喷水系统进行评估。
机译:氢隧穿作为水振动动力学参与水化学研究的探索?
机译:水隧道先进隐形飞机的静态和动态空调测试
机译:通过涡旋操纵对Nasp型车辆的气动控制。第1卷:静水隧道测试