forebody中文是什么意思

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用"forebody"造句"forebody"怎么读"forebody" in a sentence

中文翻译手机版

n.
船身前半部；水上飞机的前机身；弹体前部。

"axisymmetrical forebody" 中文翻译 : 轴对称形前机身
"chined forebody" 中文翻译 : 带边条的前机身
"ducted forebody" 中文翻译 : 函道形前机身
"forebody blowing" 中文翻译 : 自头部吹入
"forebody chine" 中文翻译 : 前机身边条
"forebody entrance" 中文翻译 : 进流段
"forebody instability" 中文翻译 : 前机身引起的不安全性
"forebody length" 中文翻译 : 前体长度
"forebody strake" 中文翻译 : 前机身边条
"forebody volume" 中文翻译 : 前体排水容积
"cocking up of forebody" 中文翻译 : 艏翘
"forebody lateral area" 中文翻译 : 前体中线面面积
"forebody lateral area coefficient" 中文翻译 : 前体中线面系数
"forebody lifting surface" 中文翻译 : 前体升力面
"forebody prismatic coefficient" 中文翻译 : 前体棱形系数
"forebody vertical prismatic coefficient" 中文翻译 : 前体垂向棱形系数
"forebody waterplane area" 中文翻译 : 船首水线面积
"forebody waterplane coefficient" 中文翻译 : 前体水线面面积系数
"fuselage-forebody lift" 中文翻译 : 前机身升力
"forebodings" 中文翻译 : 先兆
"foreboding" 中文翻译 : n. 预报，预示；(特指凶事的)预知，预感。
"forebode a big storm" 中文翻译 : 预示大风暴的来临
"forebode" 中文翻译 : vt. 1.预示；预知。 2.预感。 vi. 1.预言。 2.有预感。
"foreboard; fore deck" 中文翻译 : 前甲板

例句与用法

On exploring design of hypersonic forebody inlet and isolator of integrated scramjet
进气道和隔离段气动设计
Experiment study of aerodynamic interactions of projectile with jet from its forebody
弹丸前体喷流的气动力干扰实验研究
Dong guan winner way gold san electron industry co . , ltd ( which forebody was gold san cnc machine co . , ltd . )
东莞宏远高成电子实业有限公司前身是高成数控机械有限公司( goldsancncmachineco . , ltd
The effect of exit back pressure and length / height ratio of isolator on forebody / inlet flow field is analyzed and discussed in the paper
本文还研究了隔离段出口反压及隔离段长高比对进气道流场的影响。
This demonstrates that for propulsion - airframe integration , this genus of inlet would be advantageous in keeping the stability of boundary layer coming from the forebody
一体化设计时，该进气道对保持前机体来流附面层的稳定性十分有利。
Tzong - shyng leu , pong - jeu lu , and jeng - ren chang , " application of flexible micro balloon actuators for forebody aerodynamic control , " international symposium on experimental mechanics , december 2002
吕宗行,陆鹏举,张政仁, "可桡性微泡致动器在前弹体气动力控制之应用, "中国航空航太学会,高雄, 2002
The design point of the designed forebody / inlet is flight mach number m = 6 and flight attitude h = 25km . the three - ramp , mixed external and internal compression hypersonic / inlet is chosen as representative geometry to be designed . nine types of hypersonic / inlet model with difference forebody length and total turning angle are obtained that the incidence angle of the first ramp and height of isolator are given
根据飞行任务要求，以飞行马赫数6 ，飞行高度25km为设计点，给定前体预压缩角、隔离段高度，对具有不同前体长度和不同总压缩转角的带隔离段的前体进气道进行了设计。
Consultant consults - the flowers and plants tea - changes clothes - fragrant to smoke takes a bath - relaxes the volatile oil whole body affable massage - contemplates drop oil - forebody spa the affable massage - superior standard run skin - changes clothes - the flowers and plants tea dessert warm prompt : please ahead of time one day appointment , this service item does not participate puts crease in it
专业护理流程：顾问咨询品花草茶更衣香熏沐浴放松精油全身舒缓按摩冥想滴油头部spa舒缓按摩优格润肤更衣花草茶点心温馨提示：请提前一天预约，此服务项目不参与打折。
With account for the effect of temperature and shock - boundary layer interaction , the forebody / inlet with plane lip and wedge lip are designed by using the design methods of constant shock wave intensity and constant shock wave angle . in the design , the incidence angle of the first ramp , height of isolator , length of forebody and total turning angle of the designed forebody / inlet models are given
另外，根据优选结果，给定前体长度、前体预压缩楔角、总压缩转角及隔离段高度，分别用等激波强度和等激波角度的方法设计了唇口平直和唇口带楔角的前体进气道。
The calculation results indicate that the starting performance of forebody / inlet with wedge - shaped lip is better than that with plane lip at low flight mach number . at high flight mach number , the performance of the forebody / inlets designed by the two methods is approximate . at low flight mach number , the starting performance of forebody / inlet designed by the method of constant shock wave intensity is better
结果表明：唇口带楔角的进气道在低飞行马赫数下的起动性能优于唇口平直的进气道；采用等激波强度和等激波角度方法设计的进气道在高飞行马赫数下的性能相近，在低飞行马赫数下，采用等激波强度方法设计的进气道起动性能较优。