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增升减阻一直是空气动力设计工作者追求的目标。
The unique aim of aerodynamic designer is always to enhance lift coefficient and reduce drag coefficient.
应用数值方法模拟了飞行器升力面下表面喷气的增升作用。
The aerodynamic characteristics of an airfoil with a jet issuing from its lower surface are investigated by numerical method.
本文使用数值模拟方法研究了吸气效应对分离的控制及增升作用。
The suction effect on separation and lift force are studied by numerical method.
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