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Experimental study of wind load on a container crane located in a uniform flow and atmospheric boundary layers
The effects of oncoming atmospheric boundary layers and boom position on wind load acting on a container crane were tested in this study. A 1/150 scale-downed model of a container crane was embedded in a wind-tunnel test section. The wind environment nearby the container crane located in a port was...
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Published in: | Engineering structures 2008-07, Vol.30 (7), p.1913-1921 |
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Main Authors: | , |
Format: | Article |
Language: | English |
Subjects: | |
Citations: | Items that this one cites Items that cite this one |
Online Access: | Get full text |
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Summary: | The effects of oncoming atmospheric boundary layers and boom position on wind load acting on a container crane were tested in this study. A 1/150 scale-downed model of a container crane was embedded in a wind-tunnel test section. The wind environment nearby the container crane located in a port was simulated as a uniform flow and two types of atmospheric boundary layer (ABL) for an open coast
(
n
=
1
/
10
)
and an open terrain
(
n
=
1
/
7
)
. Wind load acting on the container crane model was measured using a 7-component balance with varying wind directions (yaw angle). Reynolds number effect on the aerodynamic coefficients was investigated with varying Reynolds number. Drag and pitching-moment coefficients have maximum values at the yaw angles of
θ
=
±
3
0
∘
, ±150
∘, and minimum values at
θ
=
±
9
0
∘
. For the simulated ABL conditions, the drag coefficient is reduced about 19%–25% on the average, compared to that in a uniform flow. However, the pitching moment in ABLs is about 10% on the average larger than that of a uniform flow. As the yaw angle increases, the drag and pitching-moment coefficients at boom-up condition are increased about 9%–14% and 37%–44%, respectively, compared with those in boom-down condition. In addition, the maximum wind load is reduced about 14% in the case of open-coast ABL and about 20% for the open-terrain ABL, compared to that in a uniform flow. |
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ISSN: | 0141-0296 1873-7323 |
DOI: | 10.1016/j.engstruct.2007.12.013 |