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Shock and Vibration
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2019
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Article
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Tab 2
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Research Article
Adaptability of Turbulence Models for Pantograph Aerodynamic Noise Simulation
Table 2
Percentage of
of the four models relative to LES (unit: %).
SAS
IDDES sst-kω
DDES sst-kω
DDES R-kε
Bottom frame area
26.4
11.4
4.6
2.5
Middle area
57.4
49.4
32.7
12.4
Panhead area
66.9
41.4
33.1
16.9