助手标题  
全文文献 工具书 数字 学术定义 翻译助手 学术趋势 更多
查询帮助
意见反馈
   航空风洞 的翻译结果: 查询用时:0.177秒
图标索引 在分类学科中查询
所有学科
航空航天科学与工程
更多类别查询

图标索引 历史查询
 

航空风洞
相关语句
  aeronautical wind tunnel
     Atmospheric Boundary Layer Simulation in a 1.4m Aeronautical Wind Tunnel
     在1.4米航空风洞中模拟大气边界层
短句来源
     The Simulation of the Atmospheric Boundary Layer in an Aeronautical Wind Tunnel
     航空风洞中大气边界层的模拟
短句来源
     Simulated fields of atmospheric boundary layers are made in 4 m×3 m aeronautical wind tunnel by properly prolonging length of the test section and by using barrier, spires, rough elements. The mean velocity profiles, turbulence intensity profiles and fluctuating wind spectra have been measured.
     通过适当地延长风洞的试验段长度,并利用尖塔、挡板、粗糙元等边界层发生装置,在4m×3m航空风洞中模拟建立了大气边界层流场,测量了模拟流场的平均风速剖面、湍流强度剖面、风谱等.
短句来源
     THE SIMULATION OF THE ATMOSPHERIC BOUNDARY LAYER IN AN AERONAUTICAL WIND TUNNEL
     航空风洞中大气边界层的模拟
短句来源
     TECHNOLOGY RESEARCHES ABOUT MODIFYING AERONAUTICAL WIND TUNNEL FOR AERODYNAMIC TESTS OF AUTOMOBILE MODELS
     关于改造航空风洞为汽车试验风洞的技术探讨
短句来源
更多       
  “航空风洞”译为未确定词的双语例句
     On Modifying a Wind-Tunnel for Airplanes to be used for Automobiles.
     关于改造航空风洞为汽车试验风洞的技术探讨
短句来源
     The van-body truck is a blunt body with irregular shape. This paper first deals with many problems in experimental technique whose solutions are prerequisite for performance experiment on aerodynamic characteristics in a mini-type aviation wind tunnel of 1-meter magnitude.
     厢式货车是一形状不规则的钝头物体,利用1米量级的小型航空风洞进行空气动力性能试验,在试验技术上有许多需要事前解决的问题。
短句来源
     This dissertation is mainly discussed in the following perspectives: coach aerodynamics shaping orderliness, coach shaping design method, using CATIA to form the numerical modeling of coach body surface according to measured points data and wind tunnel test for coach model in aviation wind tunnel.
     本课题主要在客车空气动力学造型规律、客车造型设计方法、利用CATIA软件以三坐标测量数据构建客车车身数值模型和利用航空风洞进行客车模型风洞试验等方面进行了研究。
短句来源
     Based on the review of the various artificial accelerated growth methods for boundary layer in aeronautical wind tunnels, this paper suggests a simulated device suitable for NH-2 model wind tunnel to produce atmospheric boundary layer and gives its experimental results.
     本文在评述航空风洞中各种人工加速形成边界层方法曲基础上,提出一种适用于NH-2模型风洞形成大气边界层的模拟装置及其试验结果。
短句来源
     Based on the review of the various artificial acceleratedgrowth methods for boundary layer in aeronauticalwind tunnel,this pap-er suggests a simulated equipment which is suitable for NH-2 modelwind tunnel to generate atmospheric boundary layer and its experimentresults.
     本文在评述航空风洞中各种人工加速形成边界层方法的基础上,提出一种适用于 NH-2模型风洞形成大气边界层的模拟装置及其试验结果。
短句来源
更多       
  相似匹配句对
     The Simulation of the Atmospheric Boundary Layer in an Aeronautical Wind Tunnel
     航空风洞中大气边界层的模拟
短句来源
     THE SIMULATION OF THE ATMOSPHERIC BOUNDARY LAYER IN AN AERONAUTICAL WIND TUNNEL
     航空风洞中大气边界层的模拟
短句来源
     Aerial Radiological Survey
     航空放射性测量
短句来源
     AVIATION & SPACEFLIGHT
     航空航天
短句来源
     Experimental Verification of Wind Tunnel
     风洞的实验标定
短句来源
查询“航空风洞”译词为用户自定义的双语例句

    我想查看译文中含有:的双语例句
例句
没有找到相关例句


Based on the review of the various artificial accelerated growth methods for boundary layer in aeronautical wind tunnels, this paper suggests a simulated device suitable for NH-2 model wind tunnel to produce atmospheric boundary layer and gives its experimental results.The experimental results, compared with the data from some related references, are in good agreement, so the Simulated device can be extended to NH-2 aeronautical wind tunnel for wind engineering tests.

本文在评述航空风洞中各种人工加速形成边界层方法曲基础上,提出一种适用于NH-2模型风洞形成大气边界层的模拟装置及其试验结果。试验结果与有关资料比较是相符的。故此模拟装置可推广应用到NH-2航空风洞中的风力工程试验。

Based on the review of the various artificial acceleratedgrowth methods for boundary layer in aeronauticalwind tunnel,this pap-er suggests a simulated equipment which is suitable for NH-2 modelwind tunnel to generate atmospheric boundary layer and its experimentresults.The experiment results compared with data from some related refe-rences are in good agreement,so that these simulated equipments can beextended to NH-2 aeronautical wind tunnel to use for wind engineeringtest.

本文在评述航空风洞中各种人工加速形成边界层方法的基础上,提出一种适用于 NH-2模型风洞形成大气边界层的模拟装置及其试验结果。试验结果与有关资料比较是相符的。故此模拟装置可推广应用到 NH-2航空风洞中的风工程试验中。

In this paper the classification of automotive testing wind-tunnels and the construction of some typical testing wind-tunnels overseas exclusirely for motor vehicles are presented. And some problems in modifying a windtunnel for airplanes to be used for automobile testing are analysed and discussed. Then a case of modifying the FD-09 airplane wind-tunne for automobile testig, as well as its application after modification are described.

在介绍汽车试验风洞的分类及国外一些典型的汽车专用试验风洞的结构的基础上,对改造航空风洞为汽车试验风洞时的主要问题进行了分析探讨,并介绍了改造情况及改造后的功用。

 
<< 更多相关文摘    
图标索引 相关查询

 


 
CNKI小工具
在英文学术搜索中查有关航空风洞的内容
在知识搜索中查有关航空风洞的内容
在数字搜索中查有关航空风洞的内容
在概念知识元中查有关航空风洞的内容
在学术趋势中查有关航空风洞的内容
 
 

CNKI主页设CNKI翻译助手为主页 | 收藏CNKI翻译助手 | 广告服务 | 英文学术搜索
版权图标  2008 CNKI-中国知网
京ICP证040431号 互联网出版许可证 新出网证(京)字008号
北京市公安局海淀分局 备案号:110 1081725
版权图标 2008中国知网(cnki) 中国学术期刊(光盘版)电子杂志社