scholarly journals Micro-topographic analysis of shell pavements formed by aeolian transport in a wind tunnel simulation

2012 ◽  
Vol 117 (F4) ◽  
pp. n/a-n/a ◽  
Author(s):  
Cheryl McKenna Neuman ◽  
Bailiang Li ◽  
David Nash
Keyword(s):  
Wind Tunnel ◽  
Aeolian Transport ◽  
Topographic Analysis ◽  
Wind Tunnel Simulation

scholarly journals Effects of gravel mulch on aeolian transport: a field wind tunnel simulation

2015 ◽  
Vol 7 (3) ◽  
pp. 296-303 ◽  
Author(s):  
KeCun Zhang ◽  
WeiMin Zhang ◽  
LiHai Tan ◽  
ZhiShan An ◽  
Hao Zhang
Keyword(s):  
Wind Tunnel ◽  
Aeolian Transport ◽  
Wind Tunnel Simulation ◽  
Gravel Mulch

A new atmospheric boundary layer wind tunnel simulation methodology for wind effects on large cooling towers considering wind environment variations

2018 ◽  
Vol 22 (5) ◽  
pp. 1194-1210 ◽  
Author(s):  
XX Cheng ◽  
X Chen ◽  
YJ Ge ◽  
H Jiang ◽  
L Zhao
Keyword(s):  
Boundary Layer ◽  
Wind Tunnel ◽  
Atmospheric Boundary Layer ◽  
Model Test ◽  
Test Results ◽  
Wind Effects ◽  
Simulation Methodology ◽  
Codes Of Practice ◽  
Wind Tunnel Simulation ◽  
Tunnel Model

The traditional atmospheric boundary layer wind tunnel model test practice employs wind fields, the flow characteristics of which are in accordance with the empirical formulae of the atmospheric turbulence presented in Codes of Practice and monographs. However, the empirical formulae presented in Codes of Practice and monographs cannot truthfully reflect the high variations of the realistic atmospheric turbulence which sometimes aggravates wind effects on structures. Based on model tests conducted in a multiple-fan actively controlled wind tunnel, it is found that most wind effects on large cooling towers change monotonically with the increase in free-stream turbulence, and the model test results are more unfavorable for a flow field of low turbulence intensity than for a flow field of high turbulence intensity with respect to the measured coherences. Thus, a new atmospheric boundary layer wind tunnel simulation methodology for wind effects on circular cylindrical structures is proposed to overcome the deficiency of the traditional atmospheric boundary layer wind tunnel model tests. The new simulation methodology includes the simulation of two realistic atmospheric boundary layer flow fields with the highest and the lowest turbulence intensities in the wind tunnel and the envelopment of model test results obtained in the two flow fields (e.g. the mean and fluctuating wind pressure distributions, the power spectral density, the coherence function, and the correlation coefficient). The superiority of the new atmospheric boundary layer wind tunnel simulation methodology over the traditional model test practice is demonstrated by comparing the model test results with the full-scale measurement data.

A wind tunnel simulation of the mean velocity fields behind upright porous fences

2007 ◽  
Vol 146 (1-2) ◽  
pp. 82-93 ◽  
Author(s):  
Zhibao Dong ◽  
Wanyin Luo ◽  
Guangqiang Qian ◽  
Hongtao Wang
Keyword(s):  
Wind Tunnel ◽  
Velocity Fields ◽  
Mean Velocity ◽  
Wind Tunnel Simulation ◽  
The Mean

Wind‐tunnel Simulation and Assessment of Ammonia Volatilization from Ponded Water 1

1981 ◽  
Vol 73 (3) ◽  
pp. 546-552 ◽  
Author(s):  
Reinier J. B. Bouwmeester ◽  
Paul L. G. Vlek
Keyword(s):  
Wind Tunnel ◽  
Ammonia Volatilization ◽  
Wind Tunnel Simulation

In the Wind Tunnel Simulation Defroster Control Study

2013 ◽  
Vol 380-384 ◽  
pp. 191-194
Author(s):  
Qin Yu Yang ◽  
Jin Bo Yao ◽  
Yue Ming Yang ◽  
Xue Wei Liu
Keyword(s):  
Wind Tunnel ◽  
External Environment ◽  
Aerodynamic Performance ◽  
The Body ◽  
Flight Safety ◽  
Aircraft Icing ◽  
Real Situation ◽  
Wind Tunnel Simulation ◽  
Performance Deterioration ◽  
Control Study

Aircraft in flight, such as supercooled water droplets encountered icing conditions suitable for the external environment, the relevant parts of the body will freeze, making the aircraft's aerodynamic performance deterioration, severe endanger flight safety, in addition, the aircraft parked in the open winter months , there will be icing, you need to clean up before takeoff. We should grasp the mechanism of aircraft icing, environmental factors and easy to freeze parts of the body. This paper presents a simulation using the wind tunnel icing device icing wind tunnel simulations can reproduce the real situation of aircraft icing, for guiding practice and got good results.

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