迎角风洞试验技术是先进高机动飞行器研制必需的关键技术。
High Angle of attack wind tunnel test techniques is necessary for development of high-maneuverability flight vehicles.
研究目的是探索微型飞机的风洞试验技术和获得各种微型飞机布局的低雷诺数气动特性。
The aim is to explore the experimental technique of the MAVs and obtain low Reynolds number aerodynamic characteristics on the configurations.
相变热图试验技术是通过在飞行器表面喷涂具有一定相变温度的相变涂料来进行大面积热测绘的一项风洞试验技术。
The phase change thermography technique is a wind tunnel test technique to spray some phase change paint on the aircraft surface for measuring heat distribution in a large area.
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