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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2020
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Article
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Fig 6
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Research Article
Numerical Investigation of the Wake Vortex-Related Flow Mechanisms in Transonic Turbines
Figure 6
Dimensionless density gradient contours of flow condition MUR129: (a) present SAS result; (b) LES result [
9
].
(a)
(b)