风洞试验结果的英文

• wind tunnel test-result

• "风洞"英文翻译    wind tunnel; air tunnel; whi ...
• "试验结果"英文翻译    test result
• "按风洞试验结果估算" 英文翻译 :    wind-tunnel evaluation
• "风洞与飞行试验结果比较" 英文翻译 :    tunnel-flight comparison
• "风洞试验" 英文翻译 :    wind tu el test; wind tunnel experiment; wind tunnel testing; wind tunnel trial
• "风洞试验段" 英文翻译 :    experiment chamber; experimental chamber of wind tunnel; test chamber; test section of a wind tunnel; throat
• "风洞试验室" 英文翻译 :    wind tunnel laboratory
• "热风洞试验" 英文翻译 :    hot tunnel climatic test
• "试验结果" 英文翻译 :    end of test; experimental results; test figure; test findings; test results; tested results; testing result
• "低速风洞试验" 英文翻译 :    low-speed tunnel test
• "风洞试验计划" 英文翻译 :    wind-tunnel program
• "高速风洞试验" 英文翻译 :    high-speed wind-tunnel test
• "天线风洞试验" 英文翻译 :    antenna test in tunnel
• "模拟试验结果" 英文翻译 :    analog reslt
• "盆栽试验结果" 英文翻译 :    results from pot experiment test
• "试验结果记录" 英文翻译 :    logging
• "试验结果评价" 英文翻译 :    evaluation of test result
• "试验结果阴性" 英文翻译 :    negative
• "水压试验结果" 英文翻译 :    result of hydraulic test
• "野外试验结果" 英文翻译 :    field results
• "闭式风洞试验段" 英文翻译 :    cloxed wind-runnel throat
• "风洞试验段半径" 英文翻译 :    wind tunnel radius; wind-tunnel radius
• "风洞试验段截面积" 英文翻译 :    wind-tunnel working section area
• "风洞试验段压力" 英文翻译 :    working section pressure
• "风洞试验数据处理" 英文翻译 :    wind-tunnel data reduction

• Then two - vehicle platoon in 5 different inter - vehicle distances and 3 , 4 , 5 , 6 and 7 - vehicle platoon with fixed spacing are also simulated and analyzed respectively
  研究表明：单辆车数值模拟结果与风洞试验结果基本吻合。
• In the paper , the computational results of all models are obtained , including 3 - d velocity field , 3 - d pressure field , and six aerodynamic coefficients . the results have good agreement with wind tunnel test
  文中得出了客车外围流场的速度矢量图和压力分布图以及六个气动力系数，并将最终结果与风洞试验结果进行了比较，结果吻合较好。
• Based on the results of the wind tunnel test , the response of the structure and the wind pressure distribution of different position are gotten . the evaluation of the safety and the comfortable extent under the wind vibration are achieved
  根据风洞试验结果得到结构不同部位的风压分布以及结构在风载下的响应，确定对结构安全度的评估，实现风振下结构舒适度的验算。
• It is indicated that the grids generated by the proposed method are simple , high quality and suitable for different building shapes , and the results of numerical simulation agree well those of the wind tunnel test
  网格剖分和数值模拟结果表明，采用本文方法生成的网格格式简单，网格质量高，适应性强，适用于多种体型建筑物的模拟计算，并且风场模拟结果与风洞试验结果有较好的吻合。
• In order to study the effect of the number of vehicle and inter - vehicle distance on the aerodynamic characteristics of vehicle platoon in intelligent transportation systems ( its ) , a single vehicle is simulated first and its results are compared with that of wind tunnel test
  摘要为了研究车辆前后间距和车辆数目对智能交通系统中队列行驶车辆气动特性的影响，首先对单辆车进行数值模拟，并将模拟结果与风洞试验结果进行对比，然后对两辆车在5种不同间距下以及3 ~ 7辆车在固定间距下队列行驶的情况分别进行了数值模拟及分析。
• Using the program the wind fields around several buildings with different body shapes are analyzed . the final results of grid division and refinement are presented . the final wind velocities around the building and wind pressures on the building surface are obtained and also compared with those from the wind runnel test
  采用计算程序对几种不同体型建筑物的流动风场进行了模拟计算，给出了计算区域的网格剖分和加密结果，获得了离散后的流场的风速和风压模拟结果，并与风洞试验结果进行了比较。
• Also longitudinal aerodynamic characteristics of missile are investigated . the traditional dependence on wind tunnel experiment is changed greatly : firstly , the aerodynamic characteristics of missiles with complex configuration are solved satisfactorily , especially integral rocket - ramjet missile ; secondly , feasibility of n - s equation to numerical simulation of inner and outer fiowfield of missile with complex configuration is discussed
  ( 3 )采用n - s方程方法数值模拟某型整体式冲压发动机导弹的全弹内外流场，研究了导弹的纵向气动特性，改变了过去依赖于地面风洞试验结果的传统做法。
• Using the developed computer program the wind flow around a cubic building model , a rectangle - section tall building and a gable - roof building are first numerical predicted , respectively . in the prediction the single - area and multi - area grid refinement approaches are respectively used and the numerical results are compared with the wind - tunnel test results and the numerical results without grid refinement obtained by other researchers . this indicates that the proposed nonstaggered grid and refinement scheme is not only valid and easy to be car
  采用编制的计算程序首先对一立方体建筑模型、一矩形截面高层建筑和一双坡屋面建筑的绕流风场进行了模拟计算，分别采用单域和多域加密方案对建筑周围的网格实施了局部加密，数值模拟结果与风洞试验结果以及其他研究者的非加密计算结果进行了比较。