.专业整理.
outwards from small to big to the end. The gas in the rocket
body by the front half of the high pressure into the nozzle,
through the narrow throat to escape by the rear half. This
architecture allows the speed of the air flow changes due to
changes in the jet cross-sectional area, the airflow from
subsonic to the speed of sound, until accelerated to transonic.
So, people flared nozzle called transonic nozzle. Since it was
invented by the Swedish Laval, also known as Laval nozzle.
Analysis of the principle of the Laval nozzle. The rocket
engines of the gas flow in the combustion chamber under pressure,
after the backward movement of the nozzle into the nozzle . At
this stage, the gas movement follow the principle of "the fluid
moves in the tube , the small cross-section at the flow rate
large sectional large flow velocity", thus accelerating
airflow.
Laval nozzle
When you reach the narrow throat, the flow rate has exceeded
.学习帮手.
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