Abstract <p>The results of eddy-resolving ILES simulation of turbulent mixed convection in a rapidly rotating annular cavity with a central shaft under the conditions of the well-known experiment (Bohn, 2000) are given. The cavity is heated from the disk surfaces and from the periphery, while the cooling air flows through a narrow annular channel along the shaft. The use of a relatively fine computational grid (approximately 9 million hexahedral cells concentrating toward the walls) ensured acceptable resolution of thin quasi-laminar Ekman layers and small-scale eddies, that play an important role in the heat transfer processes near the disks. A particular attention is given to the formation of realistic flow conditions at the cavity inlet (including the presence of turbulent content), taking into account the characteristics of the cooling air supply duct of the experimental facility. The proposed modification of the boundary conditions led to a dramatic improvement in the quality of heat transfer calculations in the near-axial region of the disk as compared to calculations without turbulent content at the cavity inlet.</p>

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Eddy-Resolving Numerical Simulation of Mixed Convection in a Rotating Annular Heated Cavity with Axial Throughflow

  • D. K. Zaitsev,
  • A. M. Levchenya,
  • E. M. Smirnov

摘要

Abstract

The results of eddy-resolving ILES simulation of turbulent mixed convection in a rapidly rotating annular cavity with a central shaft under the conditions of the well-known experiment (Bohn, 2000) are given. The cavity is heated from the disk surfaces and from the periphery, while the cooling air flows through a narrow annular channel along the shaft. The use of a relatively fine computational grid (approximately 9 million hexahedral cells concentrating toward the walls) ensured acceptable resolution of thin quasi-laminar Ekman layers and small-scale eddies, that play an important role in the heat transfer processes near the disks. A particular attention is given to the formation of realistic flow conditions at the cavity inlet (including the presence of turbulent content), taking into account the characteristics of the cooling air supply duct of the experimental facility. The proposed modification of the boundary conditions led to a dramatic improvement in the quality of heat transfer calculations in the near-axial region of the disk as compared to calculations without turbulent content at the cavity inlet.