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Home > chinese-english > "nozzle area" in English

English translation for "nozzle area"

喷管截面积
喷管通路面积
喷嘴截面面积
喷嘴面积
喷嘴通流面积


Related Translations:
giant nozzle:  水枪
nozzle insert:  喷管衬套
scum nozzle:  除渣喷嘴
quenching nozzle:  喷射冷却器
reversed nozzle:  反喷嘴
nozzle screen:  喷嘴滤油网
nozzle head:  纺丝头喷嘴喷嘴头
cellar nozzle:  地窖水枪
fog nozzle:  喷雾管嘴喷雾咀喷雾口喷雾水枪喷雾嘴雾化喷咀雾化喷嘴雾喷嘴
froth nozzle:  泡沫喷口泡沫喷射器
Example Sentences:
1.Design optimization of chamber pressure and nozzle area expansion ratio of solid rocket motors
固体火箭发动机燃烧室压强及喷管扩张比优化设计
2.And the affect of nozzle pressure ratio , nozzle area ratio and geometric defected angle on the performance parameters is also investigated . 4
研究了影响矢量喷管性能的因素,研究了压比、面积比以及几何偏角对矢量喷管性能的影响。
3.More than 200 different condition 3d viscosity steady flow fields in the thrust vectoring nozzle at different nozzle pressure ratio and different nozzle area ratio and different geometric defected angle is calculated by the program developed . and the related performance parameters are acquired by numerical simulation
利用该程序计算了某矢量喷管在不同的压比、面积比和几何偏转角下的200多种三维有粘流场,获得了矢量喷管的性能数据。
4.Cfd is also used to get the data of performance parameters of the nozzle at different nozzle pressure ratio , different nozzle area ratio and different geometric defected angle . the theory of function approximation is used to establish the transient model of thrust vectoring with the data calculated
本文通过cfd计算获得矢量喷管的性能参数,如流量系数、推力系数以及有效推力矢量角等与矢量喷管压比、面积比以及几何偏转角之间的关系数据,并利用函数逼近理论建立了矢量喷管的动态数学模型。
5.To meet the needs for wider surge margin of the turbofan engine , a new model was developed to predict the characteristics of the fan / high pressure compressor and turbine in this thesis . several ways , including , variable inlet guide vanes of the fan , variable guide vanes of the high pressure compressor , the variable inlet area ratio of the mixer and the nozzle areas , were presented to enlarge the surge margin of the turbofan engine . meanwhile , a method of combined variable geometries for optimizing controls of inlet guide vanes of the fan , guide vanes and the first two stators of high pressure compressor , area ratio of mixer and noz zle areas was established
为了满足下一代作战飞机对推进系统的性能和稳定性要求,本文建立了压缩系统特性和涡轮特性的新模型,并分别采用改变涡扇发动机风扇进口导流叶片、压气机导流叶片和前两级静叶片、混合室进口处内、外涵面积比和尾喷管面积,研究了其对发动机性能和稳定性的影响,进而得出了涡扇发动机变几何扩稳的方法,为发动机变几何扩稳研究打下理论基础。
Similar Words:
"nozzle aerator" English translation, "nozzle air bleed" English translation, "nozzle and socket list" English translation, "nozzle angle" English translation, "nozzle aperture" English translation, "nozzle area coefficient" English translation, "nozzle area control system" English translation, "nozzle area expansion ratio" English translation, "nozzle area ratio" English translation, "nozzle aspirating system" English translation