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Prediction of total pressure characteristics in the settling chamber of a supersonic blowdown wind tunnel

机译:超音速排污风洞沉降室内总压特性的预测

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摘要

In the design of control system of a wind tunnel, it is important to understand the importance of operations of mechanical systems in order to ensure that any emergencies that may arise during the running of the wind tunnel are properly handled by the system. In the NAL 0.6m blowdown wind tunnel, it is proposed to incorporate a Variable Mach number Flexible Nozzle (VMFN), using which the tunnel13; can be started at a low Mach number and the required test Mach number (up to 4) can be reached by continuously (on-line) changing the nozzle contour using an Electroservohydraulic drive. Before stopping the tunnel, the VMFN would be reverted to the initial low Mach number condition. During the entire operation of the tunnel in such a scenario, it is essential that the Pressure Regulating Valve (PRV) maintains the specified or minimum stagnation pressure in the test section by following a safe trajectory. In order to determine a safe trajectory, a basic understanding of the variation of stagnation pressure in the settling chamber is called for, before the PRV control system is designed. In this paper, the problem is13; formulated based on quasi-steady isentropic equations and programmed in C language to predict the timehistories13; of settling chamber pressure and storage tank pressure for a given trajectory of the opening of PRV, as the VMFN throat is changed from Mach 1 to Mach 4 condition and vice versa. In order to validate the present methodology, the PRV trajectory measured during an experiment in the NAL 0.6m13; wind tunnel was used as input to the program and the measured time-histories of settling chamber pressure and storage tank pressure are compared with the predicted values. Predictions of settling chamber pressure and the storage tank pressure relevant to VMFN operation indicate that settling chamber pressure rapidly builds up towards the storage tank pressure, apparently due to the constriction offered at the VMFN throat as VMFN throat is changed from M=1 contour to M=4 contour during the13; start of the run. Minimum PRV opening area has been predicted to maintain the settling chamber pressure13; higher than the estimated minimum value at high Mach numbers. For smaller openings of the PRV (0.065m2), the predicted pressure falls below the minimum and is hence unsafe. From the predicted time history of free-stream dynamic pressure (q), it is noted that alarming increase in q can occur during starting and stopping transients, which can damage a test model in the tunnel, balance and such other components. Therefore, the design of test object and support system need to be adequately designed.
机译:在风洞控制系统的设计中,重要的是要了解机械系统操作的重要性,以确保系统正确处理风洞运行过程中可能出现的任何紧急情况。在NAL 0.6m排污风洞中,建议采用可变马赫数柔性喷嘴(VMFN),使用该隧道13;可以以低马赫数开始,并且可以通过使用电动液压驱动器连续(在线)更改喷嘴轮廓来达到所需的测试马赫数(最多4)。在停止隧道之前,VMFN将恢复为初始低马赫数条件。在这种情况下,在隧道的整个运行过程中,至关重要的是,调压阀(PRV)应遵循安全轨迹,在测试区域内保持规定的或最小的停滞压力。为了确定安全的轨迹,在设计PRV控制系统之前,需要对沉降室内滞止压力的变化有基本的了解。本文的问题是13。基于准稳态等熵方程式制定并用C语言编程以预测时间历史13;当VMFN喉咙从1马赫变到4马赫,反之亦然时,PRV的给定轨迹的沉降室压力和储罐压力的变化。为了验证本方法,在实验中在NAL 0.6m13中测量了PRV轨迹;使用风洞作为程序的输入,并将测得的沉降室压力和储罐压力的时间历史与预测值进行比较。与VMFN运行有关的沉降室压力和储罐压力的预测表明沉降室压力迅速朝着储罐压力增加,这显然是由于VMFN喉管从M = 1轮廓变为M时VMFN喉管提供的收缩在13期间= 4轮廓运行开始。预计最小PRV开口面积可保持沉降室压力13;高于在高马赫数下的估计最小值。对于较小的PRV开口(<0.065m2),预计压力会低于最小值,因此是不安全的。从预测的自由流动压(q)的时间历程中,可以注意到在启动和停止瞬变期间q的警惕增加可能会发生,这可能会损坏隧道,天平和其他组件中的测试模型。因此,需要适当设计测试对象和支持系统的设计。

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  • 年度 2011
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  • 正文语种 {"code":"en","name":"english","id":9}
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