avidic | واژه نامه | Con-di nozzle | | اویدیک |واژه نامه هوانوردی |Aviation
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Con-di nozzle

توضیح فارسی

مجرای همگرا- واگرای موتور جت برای تغییر سرعت گازهای سوخته شده درون جت

Description

Con-di nozzle (de Laval nozzle or convergent-divergent nozzle,or CD nozzle) is a tube that is pinched in the middle, making a carefully balanced, asymmetric hourglass shape. It is used to accelerate a hot, pressurized gas passing through it to a higher speed in the axial (thrust) direction, by converting the heat energy of the flow into kinetic energy. Because of this, the nozzle is widely used in some types of steam turbines and rocket engine nozzles. It also sees use in supersonic jet engines.