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MITIGATING TRANSONIC SHOCK WAVE WITH PLASMA HEATING ELEMENTS

机译:等离子体加热元件缓解跨音速冲击波

摘要

Systems and methods for enhancing operations of an aircraft may include a plasma generator, a sensor, and a controller. The plasma generator may be positioned on an exterior of the aircraft such that it can provide localized heating thereon. The sensor may be configured to sense and transmit information regarding a transonic flight condition such as speed to the controller. The controller may be configured to activate the plasma generator in response to information from the sensor, so as to mitigate a transonic shock wave through localized heating.
机译:用于增强飞机的操作的系统和方法可以包括等离子体发生器,传感器和控制器。等离子体发生器可以定位在飞机的外部,使得其可以在其上提供局部加热。传感器可以被配置为感测关于跨音速飞行状况的信息并将诸如速度的信息传输至控制器。控制器可以被配置为响应于来自传感器的信息来激活等离子体发生器,以便通过局部加热来减轻跨音速冲击波。

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