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METHOD AND DEVICE FOR INFLUENCING THE BODY LIMIT LAYER IN A FLOW

机译:影响流动中身体极限层的方法和装置

摘要

INFLUENCE ACCORDING TO THE PRINCIPLE OF ACTIVE MODIFICATION OF THE ORIGINAL MOVEMENT OF FLOWING PARTICLES CLOSE TO THE WALL. /P P THE PHYSICAL QUANTITY OF THE FLOW TO INFLUENCE AND USES CONTINUOUSLY BY PASSIVE SENSORS. CI AS ENTRY SIGNAL IN A REGULATION CIRCUIT WHOSE OUTPUT DELIVERS AN OSCILLATION SIGNAL TO BE INTRODUCED IN THE BOUNDARY LAYER BY AN ACTIVE OSCILLATION GENERATOR; THE DEVICE CONTAINS, INSIDE THE SURFACE 5 OF THE BODY 6 SURROUNDED BY THE FLUID, AT LEAST ONE PASSIVE SENSOR ELEMENT 1, 3, 4 AND AN OSCILLATION GENERATOR 2 WHICH COOPERATE WITH AN ANALYSIS AND REGULATION CIRCUIT 7 IN SUCH A WAY THAT FROM A FLOW QUANTITY CONTINUALLY MEASURED BY THE SENSOR, THEY GENERATE INSIDE THE SAID CIRCUIT A QUANTITY OF ADJUSTMENT WHICH EXERCISES, THROUGH THE OSCILLATION TRANSMITTER 2, AN INFLUENCE OF THE DESIRED SHAPE ON THE BOUNDARY LAYER. /P P THE INVENTION APPLIES IN PARTICULAR TO SUPPORTING WING PROFILES.
机译:主动修改靠近壁的流动粒子的原始运动的原理的影响。

流量的物理量影响并通过被动传感器连续使用。 CI作为输入信号在调节电路中的输出,该输出将主动振荡发生器引入边界层的振荡信号;设备包含在包围在流体6的表面5中,至少有一个被动传感器元件1、3、4和振荡发生器2,它们通过某种方式与分析和调节电路7合作传感器连续测量的数量,它们在上述电路中通过振荡发送器2进行了适当的调整,这取决于形状对边界层的影响。

本发明尤其适用于支持机翼轮廓。

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