International Journal of Rotating Machinery / 2013 / Article / Fig 29

Review Article

Heat Transfer Augmentation Technologies for Internal Cooling of Turbine Components of Gas Turbine Engines

Figure 29

Ranges of experimental parameters for existing investigations of channel flows with rotation. (a) Rotation number versus Reynolds number. (b) Buoyancy parameter versus Reynolds number. (c) Inlet density ratio versus Reynolds number.
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275653.fig.0029b
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