1)trailing edge尾缘
1.The heat transfer and characteristics of the fluid flow in the duct with waist-shaped pin- fin arrays for the trailing edge of the turbine blade were experimentally investigated.本文对涡轮叶片尾缘中具有束腰结构扰流柱的冷却通道的传热和流动阻力特性进行了实验研究,重点研究了雷诺数、扰流柱的束腰比以及不同组合的影响。
2.Numerical methods are used to investigate the film cooling effect of turbine guide vane′s trailing edge.采用数值模拟的方法,研究了涡轮叶片尾缘斜劈缝气膜冷却的流场特性,及其对叶背面尾缘温度分布的影响。
3.In order to investigate the flow characteristics of cooling flow downstream of a turbine guide vane trailing edge slot,numerical methods of RNG k-ε turbulent model were solved.通过RNG k-ε湍流模型求解可压流的N-S方程,研究燃气轮机涡轮导向叶片尾缘劈缝出流冷气的流动情况。
英文短句/例句
1.INVESTIGATION ON INTERACTION NOISE BETWEEN STATOR WAKE AND ROTOR WITH TRAILING EDGE BLOWING静子尾缘喷气后尾迹与动叶干涉噪声研究
2.AERODYNAMIC INFLUENCE OF DIFFERENT TRAILING-EDGE CHANGING METHODS TO THE BLUNT BRAILING-EDGE AIRFOIL不同尾缘改型方式对风力机钝尾缘翼型气动性能的影响
3.A numerical study of aerodynamic characteristics of modified aerofoil with a blunt trailing edge翼型进行钝尾缘修改后气动性能的数值研究
4.Influence of Various Pin Fin Configurations on Trailing Edge Film Cooling;不同结构扰流柱对叶片尾缘气膜冷却的影响
5.A Numerical Study for the Interaction of T-S Wave and the Trailing Edge of Boundary Layer;T-S波与边界层尾缘相互作用的数值研究
6.Investigation of Trailing Edge Film Cooling by Jets Ejected from a Slot;涡轮叶片尾缘半劈缝气膜冷却实验研究
7.Numerical Study of the Augmented Cooling on the Trailing Edge of Turbine Blade;涡轮叶栅尾缘强化冷却方法的数值研究
8.Study on Aerodynamic Performance of Airfoil by Mounting a Blunt Trailing Edge to Wind Blade加装钝尾缘改善风力机桨叶气动性能的研究
9.Effect of different clapboards structure in turbine blade trailing edge complex passages on flow characteristics涡轮叶片尾缘复合通道隔板结构对流动的影响
10.Investigation on Internal Flow Field and Aeroacoustic of Turbomachinery with Trailing Edge Blowing带尾缘吹气的叶轮机械内部流动和气动噪声问题的研究
11.Caudal edges have to be straight or curving outwards, and not bending inwards.尾鳍边缘一定要直或是向外弯曲,不能向内弯折。
12.Today, the koala has climbed back from the brink of extinction and is thriving again.今天,无尾熊从绝种边缘爬了回来并且再度繁衍。
13.A decorative horizontal band, as along the upper part of a wall in a room.壁缘沿尾内墙壁的上部装饰的水平饰带
14.Position the end cap on the rear of the retainer and the outer edge of the bumper.在扣件尾部和保险杆边缘外部定位末端端盖。
15.The Individual Words in the Crevasse--on the Reason of Rewriting the Last Act of the Novel "Recorded at the Beginning of Wind and Cloud";裂隙中的个人话语——《风云初记》尾声重写缘由
16.Completeness Of Incomplete Ending --Explorations on the Ending of the Marriage of Next life;没有圆满结局的圆满——弹词《再生缘》结尾探析
17.Analysis of Clone Selective Pairing and Consanguinity Control for Seed Orchard in Pinus massoniana马尾松建园无性系选配及亲缘关系控制的分析
18.On the validity of the class Ellipura (=Parainsecta) (Hexapoda) based on the phylogenetic relationship between Collembola and Protura从弹尾纲和原尾纲的亲缘关系质疑缺尾纲(=近昆虫纲)的有效性(六足总纲)
相关短句/例句
edge blowing mixture curtain(EBMC)尾缘吹气
1.An experimental study on initial spray field of edge blowing mixture curtain(EBMC) flame holder was conducted using a particle dynamics analyzer(PDA).利用激光测雾仪(PDA)对尾缘吹气式火焰稳定器尾缘出口的初始雾化场进行了实验研究,在静止空气中测量了尾缘出口下游不同截面上的各点处的液滴直径、速度等参数,分析了雾化场结构,初步探讨了初始雾化场的特征。
3)turbine blade trailing edge叶片尾缘
1.Different structure diaphragm plates in complex passages of turbine blade trailing edge;涡轮叶片尾缘复合通道隔板结构
2.The experiment mainly aimed at to investigate the effect of different aperture in different clapboard structure in the turbine blade trailing edge complex passages on heat transfer and pressure drop characteristics.采用热色液晶测温法,测量了涡轮叶片尾缘带隔板的复合通道的温度场。
4)trailing edge modification尾缘修形
1.<Abstrcat>The numerical simulation of three dimensional internal and external flows for non-vectoring two-dimensional nozzles with or without trailing edge modification was conducted by means of time marching finite volume method.针对美国第四代战斗机F-22在二元收-扩喷管设计应用上的特点,利用时间推进的有限体积法对二元喷管尾缘修形前后非矢量状态下的内外流混合流场进行了数值模拟。
5)trailing edge loss尾缘损失
1.Calculations show that the coolant flow mass, base pressure and boundary layer momentum thickness have a great effect on the trailing edge loss.基于Denton的尾缘流动理论 ,发展了一种考虑冷气喷射的二维、可压涡轮叶栅尾缘混合损失模型 ,研究了涡轮叶栅尾缘损失的特征 ,定量评估了影响尾缘损失的各种参数。
6)trailing edge flow尾缘流动
延伸阅读
八缘──地动八缘【八缘──地动八缘】 ﹝出增一阿含经﹞ [一、因水火风动故地动],经云:此阎浮提地,南北阔二万一千由旬,东西阔七千由旬,厚六万八千由旬。地下有水,厚八万四千由旬。水下有火,厚八万四千由旬。火下有风,厚六万八千由旬。风下有金刚轮,过去诸佛舍利,咸在其中。或有时大风忽动,火亦随动。火既动已,水复随动。水既动已,地即随动。故云因水火风动故地动。(梵语阎浮提,华言胜金洲。梵语由旬,华言限量,或四十里,或六十、八十里也。) [二、菩萨处母胎故地动],经云:菩萨从兜率天降神来处母胎,是时地亦大动。(梵语兜率,华言知足。佛在兜率天时,称为菩萨。) [三、菩萨出母胎故地动],经云:菩萨出母胎时,是时地亦大动。 [四、菩萨成道故地动],经云:菩萨出家学道,成无上正觉,即名为佛,是时地亦大动。 [五、佛入涅槃故地动],梵语涅槃,华言灭度,是时地亦大动。 [六、比丘欲现神通故地动],梵语比丘,华言乞士。经云:有大神通比丘,欲现多种变化,或分一身为千百身,还复为一。飞行虚空,山石无碍,涌没自由,是时地亦大动。 [七、诸天舍本形位得作天主故地动],经云:诸天有大神通,神德无量,从彼命终,还生彼处,由佛德力,舍本天形,得作帝释,或作梵主,是时地亦大动。(帝释,梵语释提桓因,华言能天主。梵主,即梵天主也。) [八、饥馑刀兵将起故地动],经云:若众生命终福尽,或互相攻伐,或值饥馑,或遇刀兵,是时地亦大动。