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The plenum method versus blockage corrected nozzle method for determining climatic wind tunnel air speed

机译:集水法与堵塞校正喷嘴法确定气候风洞气流

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Recently, computational fluid dynamics (CFD) was applied to investigate blockage (or velocity) corrections using the nozzle method for a climatic wind tunnel (CWT) test environment (SAE 2003-01-0936). The study included two blockage corrections to the nozzle method reference velocity: vehicle frontal velocity and vehicle upper surface pressure trace. These methods resulted in well correlated predictions between the open road and CWT flow conditions. These CFD-predicted blockage corrections are experimentally verified in a climatic wind tunnel in this study. A non-intrusive method applying particle image velocimetry is applied to acquire the velocity field in front of the test vehicle. The experimental data verifies the blockage correction predictions derived from the previous CFD work. Furthermore, the verification experiment also confirms the blockage non-uniformity around the test vehicle, which emphasizes the importance of customizing blockage correction for different test objectives. The same CFD solutions and an additional CFD simulation for the same climatic wind tunnel with the empty test section were applied to explore the plenum method in the simulated climatic wind tunnel. The same local velocity curve fit procedure used to define blockage correction factors (V{sub}(actual)/V{sub}(ΔP)) in the previous nozzle method study was applied using the pressure differentials from the tunnel stilling chamber to plenum locations to derive V{sub}(ΔP). The study showed that the climatic wind tunnel plenum method is able to achieve blockage correction values close to 1.0 for both frontal velocity and surface pressure simulation cases when vehicle blockage was 60% and below. When the optimum static pressure location was selected, the blockage correction values differed from 1.0 by -2.8% to +3.1%. For the range of plenum static pressure locations investigated, this range increased to -4.7% to 5.6%. No consistent correlation curve was found that allowed these blockage corrections to be applied in a universal manner as was found in the previous nozzle method study. In the absence of such a correlation, use of the nozzle method with the unified nozzle blockage correction correlations from SAE 2003-01-0936 are considered a more accurate method for obtaining the correct effective flow velocity for climatic wind tunnel testing than using the plenum method. Frontal velocity blockage corrections for a sedan with a 76% blockage ratio positioned close to the nozzle exit did not fall into the pattern of the 60% and below blockage cases. This was also true for the previous nozzle method study. The differences between frontal velocity blockage correction factor and surface pressure blockage correction factor for this case were large for both nozzle and plenum methods. These results suggest that a minimum test D{sub}(WB) greater than 1.65 m be developed with consistency with lower blockage results as a selection criterion.
机译:最近,应用计算流体动力学(CFD)来研究使用用于气候风洞(CWT)测试环境的喷嘴方法(SAE 2003-01-0936)来研究堵塞(或速度)校正。该研究包括两个阻塞矫正喷嘴方法参考速度:车辆正速度和车辆上表面压力迹线。这些方法导致开放道路和CWT流动条件之间的良好相关预测。这些CFD预测的封闭式校正在本研究中的气候风隧道中进行了实验验证。施加施加粒子图像速度的非侵入式方法以获取测试车前面的速度场。实验数据验证源自先前的CFD工作的堵塞校正预测。此外,验证实验还证实了测试车辆周围的堵塞不均匀性,这强调了对不同测试目标定制堵塞纠正的重要性。采用相同的CFD解决方案和具有空测试部分的相同气候风洞的额外CFD模拟,以探索模拟气候风洞中的增压机方法。使用来自隧道静脉室内腔室的压差施加到预旋液研究中的堵塞校正因子(V {sub}(实际)/ v {sub}(Δp))的相同局部速度曲线拟合程序。派生v {sub}(Δp)。该研究表明,当车辆堵塞为60%及以下时,气候风隧道压力隧道能力能够实现接近1.0的堵塞校正值,接近1.0。选择最佳静压位置时,堵塞校正值从1.0差约-2.8%到+ 3.1%。对于所研究的压力静电位置的范围,该范围增加到-4.7%至5.6%。没有发现任何一致的相关曲线,其允许以普遍的方式应用这些堵塞校正,如先前的喷嘴方法研究中发现。在没有这种相关性的情况下,利用来自SAE 2003-01-0936的统一喷嘴阻塞校正相关性的喷嘴方法被认为是用于获得对气候风洞测试的正确有效流速的更准确的方法,而不是使用压力室方法。具有76%封闭率的轿车的正面速度阻塞校正靠近喷嘴出口的封闭率并未落入60%和低于堵塞情况下的模式。对于先前的喷嘴方法研究,这也是如此。对于这种情况来说,正速堵塞校正因子和表面压力阻塞校正因子的差异对于喷嘴和全部方法都很大。这些结果表明,大于1.65米的最小测试D {Sub}(WB)是以较低的封闭结果作为选择标准的一致性开发。

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