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EXPERIMENTAL INVESTIGATION OF A'CONTINUOUS YAW DATA ACQUISITION METHOD FOR GROUND VEHICLE AERODYNAMICS

机译:地面空气动力学的连续偏航数据采集方法的实验研究

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Classical methods of data acquisition in wind tunnel testing involve a "point pause" approach, where aerodynamic data is gathered over a brief time period with the model orientation and wind tunnel conditions held nominally fixed. Following acquisition of data for an appropriate interval, the model orientation (or tunnel condition) is changed relatively quickly to the next desired value(s) and the process repeated. It is generally acknowledged that this technique is relatively "slow", where a large number of model orientations or tunnel set points are to be investigated. Further, there is little possibility of detecting subtle aerodynamic anomalies occurring between the chosen set points.The possibility of acquiring aerodynamic data on a more-or-less continuous basis, with slow, typically monotonic changes in model orientation and/or tunnel conditions has therefore been a subject of investigation in the aeronautical application. The technique is referred to as "continuous sweep" or similar. No prior investigation into the use of continuous sweep data acquisition with ground vehicle testing is known to the author.An experimental investigation was therefore performed to test the feasibility of continuous data acquisition during yaw angle sweeps of a ground vehicle. The tests were performed in Old Dominion University's (ODU) Langley Full-Scale Tunnel (LFST) with an automotive balance. The LFST is a low speed, continuous return wind tunnel with a large (30 ft. by 60 ft.) open test section. The Ahmed reference model was chosen as the test subject, due to the known stability of the flow structure, and availability of previous data.The experiment shows that force data over a range of yaw angles can be attained in a shorter time period with little loss in data quality. The experiment also showed that aerodynamic details could be detected in the sweep data that would not have been possible with the classical point-pause method of data acquisition.
机译:风洞测试中的经典数据采集方法涉及“点暂停”方法,该方法在短时间内收集空气动力学数据,并保持模型方向和风洞条件名义上固定。在以适当的间隔获取数据之后,将模型方向(或隧道条件)相对快速地更改为下一个所需值,然后重复该过程。通常公认的是,该技术相对“缓慢”,其中要研究大量的模型方向或隧道设置点。此外,几乎不可能检测到在所选设定点之间发生的细微的空气动力学异常。 因此,在模型方向和/或隧道条件上缓慢或通常单调变化的情况下,或多或少连续地获取空气动力学数据的可能性已经成为航空应用中研究的主题。该技术称为“连续扫描”或类似方法。作者尚不了解在地面车辆测试中使用连续扫描数据采集的事先调查。 因此,进行了实验研究以测试在地面车辆的偏航角扫掠期间连续数据采集的可行性。测试是在具有汽车天平的Old Dominion University(ODU)兰利全尺寸隧道(LFST)中进行的。 LFST是低速连续返回风洞,具有较大的(30英尺乘60英尺)开放测试区域。由于已知流动结构的稳定性和先前数据的可用性,选择了艾哈迈德参考模型作为测试对象。 实验表明,可以在较短的时间内获得偏航角范围内的力数据,而数据质量的损失很小。实验还表明,可以在扫掠数据中检测到空气动力学细节,而经典的点暂停数据采集方法是不可能做到的。

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