Model Wind Tunnel Experiment 模型风洞试验
gun wind tunnel experiment 炮风洞实验
the wind tunnel experiment 风洞实验
hypersonic wind tunnel experiment 高超声速风洞试验
wind tunnel experiment efficiency 风洞实验效率
base bleed wind tunnel experiment 底排风洞实验
simulation of wind tunnel experiment 风洞实验模拟
aeroelastic model wind tunnel experiment 气动弹性模型风洞实验
The wind tunnel experiment.
3．模型的风洞实验研究。
参考来源 - 战斗机气动力综合设计方法研究The design of any aircraft must experiment through a great deal of wind tunnel experiment then can complete the leap from ground to air.
任何飞行器的设计，必须经过大量的风洞试验才能完成从地面到空中的飞跃。
参考来源 - 机身低速颤振模型的芯板拓扑优化How to calculate the wind load on platform structure accurately without wind tunnel experiment is a worthy issue.
因而如何在缺乏风洞试验条件的情况下,准确地计算平台结构的风荷载成为一个值得研究的问题。
参考来源 - 海洋平台上的风荷载计算研究·2,447,543篇论文数据，部分数据来源于NoteExpress
This paper introduces a wind tunnel experiment technique of side-back jet, aerodynamic interactions and predict method.
主要阐述了弹丸头部喷流风洞实验中的实验方法、动力干扰影响及预测方法。
The viscous flow around M6 wing and F4 wing-body configuration are simulated and compared with the results of wind tunnel experiment.
为了验证方法和程序的正确性，论文中对M6机翼和F4翼身组合体的流场进行了数值模拟，并与试验结果进行了对比。
Low speed wind tunnel experiment requires strict of the wind speed, which requires a wild range of wind speed, high precision, and quick adjustment.
低速风洞实验要求对实验段的风速有严格的控制，要求风速调节范围宽，精度指标高，调节速度快。
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