首页> 外国专利> METHOD FOR CONTROLLING THE BORDER LAYER OVER THE AERODYNAMIC SURFACE OF AN AIRCRAFT, AND AIRCRAFT.

METHOD FOR CONTROLLING THE BORDER LAYER OVER THE AERODYNAMIC SURFACE OF AN AIRCRAFT, AND AIRCRAFT.

机译:用于控制飞机的空气动力学表面上的边界层的方法,以及飞机。

摘要

A method for controlling the boundary layer by suction of the air from vortex chambers provided in the aft part of the aerodynamic surface of the flying vehicle (FV), wherein the speed of the air suction is regulated being first increased until the boundary layer joins the streamlined surface and then decreased until the pressure starts to drop at the aft part of the FV. An FV provided with a boundary layer control system comprising a number of vortex chambers (1) housing streamlined bodies (2) and connected by a common channel (9) through a receiver (8) to a low pressure source (4). IMAGE
机译:一种用于通过从飞行器的空气动力学表面(FV)的空气动力学表面的后部中提供的涡流室中抽吸空气来控制边界层的方法,其中,首先提高空气抽吸的速度,直到边界层加入到空气中。流线型表面,然后降低,直到FV的后部压力开始下降。一种具有边界层控制系统的FV,其包括多个涡流室(1),这些涡流室(1)容纳流线型主体(2),并通过公共通道(9)通过接收器(8)连接到低压源(4)。 <图像>

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