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A device for the simulation of the aerodynamic forces along two steerable control surfaces, such as, for example, of a missile

机译:用于模拟沿两个可操纵控制面(例如导弹)的空气动力的装置

摘要

Device for simulation of the aerodynamic forces applied on two steerable fins of a vehicle such as a missile. & br / in order to simulate in the laboratory, the aerodynamic forces due to the lift and the deflection of the two surfaces (12) the machine (10), it is proposed a device for simulation. This device comprises two anchorage parts (16), provided to be fixed on the control surfaces (12), a system (26) of voltage, applied to the adjustable rudders a traction force simulating the lift, and two systems (28) of application of resistant torques applied independently on each of the rudders a resisting torque is proportional to its deflection.
机译:用于模拟施加在车辆(如导弹)的两个可操纵鳍上的空气动力的装置。 &为了在实验室中模拟由于机器(10)的两个表面(12)的升起和偏转而产生的空气动力,提出了一种用于模拟的装置。该装置包括两个固定在控制表面(12)上的锚固部件(16),一个电压系统(26),一个模拟升力的牵引力和两个施加系统(28)施加到可调舵上在独立地施加在每个舵上的抵抗扭矩中,抵抗扭矩与其偏转成正比。

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