Flow in injector passages of a variable thrust liquid propellant rocket engine was studied.

本文对变推力液体火箭发动机喷注器通道内介质流动进行求解。

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Flow in injector passages of a variable thrust liquid propellant rocket engine was studied.

本文对变推力液体火箭发动机喷注器通道内介质流动进行求解。

youdao