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wind tunnel

英 [ˈwɪnd tʌnl]

美 [ˈwɪnd tʌnl]

n.  (试验飞机等用的)风洞,风道

化学

牛津词典

    noun

    • (试验飞机等用的)风洞,风道
      a large tunnel where aircraft, etc. are tested by forcing air past them

      柯林斯词典

      • (尤用于测试新汽车、新飞机等的)风洞
        Awind tunnelis a room or passage through which air can be made to flow at controlled speeds. Wind tunnels are used to test new equipment or machinery, especially cars and aeroplanes.

        英英释义

        noun

        • a structure resembling a tunnel where air is blown at known velocities for testing parts of aircraft

          双语例句

          • Therefore, designers and researchers must place heavy reliance on wind tunnel testing of aeroelastic models.
            因而设计者和研究者必须高度依赖气动弹性模型风洞试验。
          • Wind tunnel tests indicate that the designed high lift system has good aerodynamics characteristics.
            风洞试验表明,改装成功的验证机增升装置具有良好的气动特性。
          • The paper introduced a spinning model surface pressure measurement sy which used in the wind tunnel.
            本文介绍了可用于测量风洞中旋转模型表面压力分布的集成测试系统。
          • Exterior flow field measurement above smooth and different riblet surfaces was carried out in a low speed wind tunnel by means of hot-wire anemometry.
            利用热线风速仪,对光滑表面和多个脊状表面在低速风洞中进行了表面流场测试。
          • NET and the design of data module in Wind Tunnel Control System.
            NET平台的风洞控制系统的通讯及数据管理模块,并介绍其开发流程。
          • That second image is very similar to the wind tunnel model I'm thinking of.
            第二副图(就是北京航展上的照片,我刚才略过了)很像我说的风洞模型。
          • An experimental modeling study executed in NJU meteorological wind tunnel was described in this paper.
            本文给出了一项在南京大学NJU环境风洞中实施的实验模拟研究。
          • This paper introduces a wind tunnel experiment technique of side-back jet, aerodynamic interactions and predict method.
            主要阐述了弹丸头部喷流风洞实验中的实验方法、动力干扰影响及预测方法。
          • Analysis of Buffeting Response for Long-span Airfoil Bridge and Research of Wind Tunnel Test
            大跨度翼型桥梁抖振响应分析及风洞试验研究
          • This paper describes the investigation of boundary layer separation control for supercritical aerofoil using micro vortex generator in the low speed wind tunnel.
            在低速风洞中研究了微型涡流发生器对超临界翼型边界层分离的控制。