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2018 Aerodynamic Measurement Technology and Ground Testing Conference最新文献

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A Spectrally-resolved Rayleigh scattering set-up to measure velocity and temperature in high-speed flows 一个光谱分辨瑞利散射装置,用于测量高速流动中的速度和温度
Pub Date : 2018-06-24 DOI: 10.2514/6.2018-2988
J. Panda, Bethany A. Drain
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引用次数: 3
Design of Torsional Test Stand for Micro-Newton Force Detection 微牛顿力检测扭转试验台的设计
Pub Date : 2018-06-24 DOI: 10.2514/6.2018-3737
Lane E. Schultz, Thomas. Cogger, Ryan Good, J. Schneider, R. Rothschild, William Nollet
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引用次数: 0
A Computational Study of Transonic Wall Interference for High Aspect Ratio Wind Tunnel Models at Sideslip Using Wings-Level-Yaw and Pitch-Roll Attitude Techniques 大展弦比风洞模型在侧滑处跨声速壁干扰的机翼水平偏航和俯仰滚转姿态计算研究
Pub Date : 2018-06-24 DOI: 10.2514/6.2018-3875
W. Schuman
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引用次数: 0
Sensors for the Measurement of Flow Induced Surface Pressure Fluctuations: Detection of Clipping and Calibration 测量流量引起的表面压力波动的传感器:检测剪切和校准
Pub Date : 2018-06-24 DOI: 10.2514/6.2018-4112
K. Stahl, F. Manegar, T. Carolus
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引用次数: 0
Stereovision Based Determination of Aerodynamic Coefficients for a Wind Tunnel Model in Free Rotational Motion 基于立体视觉的自由旋转风洞模型气动系数测定
Pub Date : 2018-06-24 DOI: 10.2514/6.2018-3804
B. Martinez, P. Wey, Michel Lisbig, Denis Bidino, M. Bastide, J. Juncker, F. Leopold
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引用次数: 0
Testing of an Autonomous Boundary Layer Data System Device in the Transonic Flight Regime 自主边界层数据系统装置在跨音速飞行状态下的测试
Pub Date : 2018-06-24 DOI: 10.2514/6.2018-4196
K. Mejia, Charles Ulk, Alexandre P. Antunes, R. Cosin, R. Westphal
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引用次数: 2
Advances in Infrared Imaging Analysis Techniques for AEDC PWT/VKF Wind Tunnel Applications AEDC PWT/VKF风洞红外成像分析技术研究进展
Pub Date : 2018-06-24 DOI: 10.2514/6.2018-4048
C. Hall
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引用次数: 0
Performance Optimization of X3R: A New Reflected Shock Tunnel Mode for the X3 Expansion Tube X3R膨胀管性能优化:一种新的反射激波隧道模式
Pub Date : 2018-06-24 DOI: 10.2514/6.2018-3563
S. Stennett, D. Gildfind, P. Jacobs, R. Morgan
Availability of reflected shock tunnels capable of testing large-scale models and producing long-duration test flows is currently limited. The X3R free-piston reflected shock tunnel is in the final stages of development as an alternate operating mode of the pre-existing X3 expansion tube at The University of Queensland. A set of analytical and numerical procedures have been developed to aid in optimization of new operating conditions. This paper summarizes the condition development process and provides details of three candidate Mach 7 operating conditions theoretically capable of generating at least 10 ms of test time for full-scale scramjet engine testing. The facility’s atypical geometry, arising from its original design as an expansion tube, and the required compromises made during condition development are discussed.
目前,能够测试大型模型和产生长时间测试流的反射激波隧道的可用性有限。X3R自由活塞反射激波隧道是昆士兰大学现有X3膨胀管的替代工作模式,目前正处于开发的最后阶段。为了帮助优化新的操作条件,已经开发了一套分析和数值程序。本文总结了条件的发展过程,并提供了理论上能够产生至少10ms试验时间的三种候选马赫7工作条件的详细信息,用于全尺寸超燃冲压发动机试验。该设施的非典型几何形状源于其最初的膨胀管设计,以及在条件开发过程中需要做出的妥协。
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引用次数: 7
Characterizing Wave Propagation in an Unsteady Transonic Wind Tunnel 非定常跨声速风洞中波传播特性研究
Pub Date : 2018-06-24 DOI: 10.2514/6.2018-3568
Wenbo Zhu, B. Harter, J. Gregory, J. Bons
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引用次数: 3
Practical Challenges in the Calculation of Turbulent Viscosity from PIV Data 基于PIV数据计算湍流粘度的实际挑战
Pub Date : 2018-06-24 DOI: 10.2514/6.2018-2987
S. Beresh, N. Miller, Barton L Smith
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引用次数: 5
期刊
2018 Aerodynamic Measurement Technology and Ground Testing Conference
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