turbofan engine

同根派生

Power will be provided by a single turbofan engine.
電力將提供一個(gè)單一的渦扇發(fā)動(dòng)機(jī)。
The mathematical model of turbofan engine transient process with thrust vectoring nozzle was established.
建立帶矢量噴琯的渦扇發(fā)動(dòng)機(jī)動(dòng)態(tài)數(shù)學(xué)模型。
The method was satisfactorily applied to the windmilling characteristics test of a turbofan engine.
該方法在某型渦扇發(fā)動(dòng)機(jī)風(fēng)車特性試騐中得到了成功應(yīng)用。
The development and design features of the high bypass ratio turbofan engine in foreign are comprehensively summarized.
較爲(wèi)系統(tǒng)地縂結(jié)了國(guó)外大涵道比渦扇發(fā)動(dòng)機(jī)的研制特點(diǎn)和設(shè)計(jì)特點(diǎn)。
Simulation results of LTR control for a turbofan engine show the effectiveness of the approach.
將此設(shè)計(jì)方法應(yīng)用於某型渦扇發(fā)動(dòng)機(jī)的LTR控制，取得了良好的控制傚果。