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Study on under-floor flow to reduce ballast flying phenomena ... - UIC

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We thought that in the downstream end the effect of the snow-accreti<strong>on</strong> reducti<strong>on</strong> was the<br />

smallest and in the area of the upper stream and center of the bogies the effect is larger.<br />

Therefore we made clear that the effect of the snow particle flux reducti<strong>on</strong> extended over large<br />

area near the bogies.<br />

SPC<br />

Deflec<strong>to</strong>r<br />

SPC<br />

Flow with snow<br />

Figure 13 Arrangement of wind tunnel tests<br />

Snow particle flux reducti<strong>on</strong><br />

(no deflec<strong>to</strong>r = 1.0)<br />

1.2<br />

1.0<br />

0.8<br />

0.6<br />

0.4<br />

0.2<br />

0<br />

Deflec<strong>to</strong>r made by equilateral<br />

triangular prisms<br />

No Def. Sd3 Sd2 Sd1<br />

Figure 14 Snow-accreti<strong>on</strong> reducti<strong>on</strong><br />

4. C<strong>on</strong>clusi<strong>on</strong><br />

We studied the <strong>under</strong>-<strong>floor</strong> <strong>flow</strong> of the car that can cause the <strong>ballast</strong> <strong>flying</strong> <strong>phenomena</strong>. Firstly,<br />

<strong>to</strong> estimate the <strong>under</strong>-<strong>floor</strong> <strong>flow</strong> <strong>under</strong> actual c<strong>on</strong>diti<strong>on</strong>s, we measured the <strong>under</strong>-<strong>floor</strong> <strong>flow</strong> in <strong>on</strong>track<br />

tests. To measure the <strong>flow</strong>, we used comb Pi<strong>to</strong>t tubes and a hot wire anemometer. The<br />

test result showed that smoothing the <strong>under</strong>-<strong>floor</strong> of the cars <strong>reduce</strong>d the <strong>under</strong>-<strong>floor</strong> <strong>flow</strong>.<br />

Sec<strong>on</strong>dly, <strong>to</strong> investigate the possibility of reducti<strong>on</strong> of the <strong>under</strong>-<strong>floor</strong> <strong>flow</strong> by modificati<strong>on</strong> of<br />

<strong>under</strong>-<strong>floor</strong> shape, we carried out wind tunnel tests by using a closed type test secti<strong>on</strong> of the<br />

Large-scale wind tunnel that has the moving-belt and the boundary layer sucti<strong>on</strong> device <strong>to</strong><br />

simulate the <strong>flow</strong> between car models and the ground. Comparing the <strong>under</strong>-<strong>floor</strong> <strong>flow</strong> in the <strong>on</strong>track<br />

tests and that in wind tunnel tests, we verified that the <strong>under</strong>-<strong>floor</strong> <strong>flow</strong> in the <strong>on</strong>-track tests<br />

was reproduced in the wind tunnel tests. We measured the velocity profiles of the <strong>under</strong>-<strong>floor</strong><br />

<strong>flow</strong> of the intermediate car by using hot wire anemometers. We <strong>under</strong>s<strong>to</strong>od that the more we<br />

smooth the <strong>under</strong>-<strong>floor</strong> shapes, the more the <strong>under</strong>-<strong>floor</strong> <strong>flow</strong> decreases. Furthermore, we<br />

developed a model running facility that enables us <strong>to</strong> estimate the velocity of the <strong>flow</strong> <strong>on</strong> the<br />

ground when the train passes by.

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