Numerical study on scale of high speed train model for wind tunnel testing

2011 ◽  
Author(s):  
Hui Zhu ◽  
Zhigang Yang
Keyword(s):  
Wind Tunnel ◽  
High Speed ◽  
Numerical Study ◽  
Wind Tunnel Testing ◽  
High Speed Train ◽  
Tunnel Testing

Comparison of different ground simulation systems on the flow around a high-speed train

2016 ◽  
Vol 231 (2) ◽  
pp. 135-147 ◽  
Author(s):  
Chao Xia ◽  
Xizhuang Shan ◽  
Zhigang Yang
Keyword(s):  
Boundary Layer ◽  
Wind Tunnel ◽  
High Speed ◽  
Separation Bubble ◽  
Adverse Pressure Gradient ◽  
Boundary Layer Separation ◽  
Wind Tunnel Testing ◽  
High Speed Train ◽  
Simulation Systems ◽  
Tunnel Testing

The influence of different ground simulation systems on the air flow around a high-speed train with zero yaw angle is investigated. Force values, force development graphs, surface pressures, the underbody flow and the wake are studied in detail with Computational Fluid Dynamics, which is initially validated by wind tunnel testing. It shows that the stationary ground has severe deviations from the full moving ground on the aerodynamic performance due to the inaccurate pressure distribution on the underbody. This is mainly attributed to the high level of interaction between the underbody and the boundary layer development. In addition, a ground boundary layer separation bubble can be observed under the tail end of the train for the stationary ground on account of insufficient energy to overcome the increasing adverse pressure gradient. In order to guarantee a correct underbody flow, a partially moving ground is proposed, including the “3-moving ground” and the “1-moving ground”. Such ground simulation systems are well compatible with the fixed rail tracks and the bottom support struts compared to the full moving ground. As a conceivable method to reduce the influence of the boundary layer, raising the high-speed train model with different ground clearances is also studied. Overall, the 3-moving ground is suggested to be the best choice for the ground simulation systems in high speed train wind tunnel testing.

A report on High Speed Wind Tunnel Testing of the Large Scale Advanced Prop-Fan

1988 ◽  
Author(s):  
P. BUSHNELL ◽  
W. CAMPBELL ◽  
H. WAINAUSKI
Keyword(s):  
Wind Tunnel ◽  
High Speed ◽  
Large Scale ◽  
Wind Tunnel Testing ◽  
Tunnel Testing

scholarly journals Surface Visualization Methods at High Speed Wind Tunnel Testing for Reentry Vehicle

1998 ◽  
Vol 18 (69) ◽  
pp. 110-116_1
Author(s):  
Kojiro SUZUKI ◽  
Tadaharu WATANUKI ◽  
Hirotoshi KUBOTA
Keyword(s):  
Wind Tunnel ◽  
High Speed ◽  
Wind Tunnel Testing ◽  
Reentry Vehicle ◽  
Surface Visualization ◽  
Tunnel Testing

Videogrammetry of the Model’s Attitude in Wind Tunnel Testing

2012 ◽  
Vol 190-191 ◽  
pp. 1273-1277 ◽  
Author(s):  
Zheng Yu Zhang ◽  
Zhong Xiang Sun ◽  
Xu Hui Huang ◽  
Yan Sun
Keyword(s):  
Standard Deviation ◽  
Wind Tunnel ◽  
Drag Coefficient ◽  
Systematic Error ◽  
Measurement System ◽  
High Speed ◽  
Wind Tunnel Test ◽  
Wind Tunnel Testing ◽  
Supersonic Wind Tunnel ◽  
Tunnel Testing

The advanced precision of drag coefficient is 0.0001 for the high speed wind tunnel test of measuring forces, the model’s angle of attack precision is ≤0.01°following errors distribution. A videogrammetric method of model’s attitude is therefore proposed, its uncertainty is investigated, and a compensation method of its systematic error is also presented by this paper. The three engineering videogrammetric experiments of attack angle in 2 meter supersonic wind tunnel testing have demonstrated that measuring standard deviation of videogrammetric measurement system established by this paper is ≤0.0094°, in addition it neither destroys the model’s shape, nor changes the stiffness or strength, so it is useful and effective.

scholarly journals Numerical Study of the Aerodynamic Characteristics of an Airfoil with Thickness Uncertainty for a Wind Tunnel Testing

2012 ◽  
Vol 40 (6) ◽  
pp. 475-484
Author(s):  
Tae-Hyeong Yi ◽  
Ki-Jung Kwon ◽  
Keun-Taek Kim ◽  
Seok-Min Ahn
Keyword(s):  
Wind Tunnel ◽  
Numerical Study ◽  
Aerodynamic Characteristics ◽  
Wind Tunnel Testing ◽  
Tunnel Testing
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