Flow Structure Transition inside Contra-Rotating Disk Cavity

Author:

Chen Shu Xian1,Shi Xue Jie1,Tan Xiao Ming2

Affiliation:

1. Civil Aviation Flight University of China

2. Nanjing University of Aeronautics and Astronautics

Abstract

The turbulent flow inside contra-rotating disk cavity was numerically studied based on the finite volume method. The flow structure and its transition characteristics inside a contra-rotating were studied. The flow structure varies with the angular velocity ratio Γ of the slower disk to that of the faster one. For Γ=-1, the Stewartson-type flow occurs throughout the domain. For Γ=0, the Batchelor-type flow occurs throughout the flow region. The stagnation streamlines originating from the stagnation point are formed for-1<Γ<0, and batchelor-type flow occurs radially outward of the stagnation point with Stewartson-type flow radially inward. The stagnation point moves radially outward as Γ is reduced.

Publisher

Trans Tech Publications, Ltd.

Reference11 articles.

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3. Ji H H, Zhang J Z, Liang B. Simulation of turbulent flow within an enclosed rotor-stator disc cavity[J]. Journal of Aerospace Power, 2001, 16(1): 13-18.

4. Cai Y, Xu G Q, Tao Z, et al. Experimental investigation of unsteady heat transfer between counter-rotating disks[J]. Journal of Aerospace Power, 2004, 19(3): 346-350.

5. Chen J X, Gan X, Owen J M. Heat transfer from air-cooled contra-rotating disks[J]. ASME Journal of Turbomachinery, 1997, 119(1): 61-67.

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