A CFD method was used to study the whole flow field in a gas centrifuge. In this paper, the VSM (Vector Splitting Method) of the FVM (Finite Volume Method) was used to solve the 3D Navier-Stokes equations. An implicit second-order upwind scheme was adopted. The numerical simulation was successfully performed on a parallel cluster computer and a convergence result was obtained. The simulation shows that: in the withdrawal chamber, a strong detached shock wave is formed in front of the scoop; as the radial position increases, the shock becomes stronger and the distance to scoop front surface is smaller. An oblique shock forms in the clearance between the scoop and the centrifuge wall; behind the shock-wave, the radially-inward motion of gas is induced because of the imbalance of the pressure gradient and the centrifugal force. In the separation chamber, a countercurrent is introduced. This indicates that CFD method can be used to study the complex three-dimensional flow field of gas centrifuges.
Skip Nav Destination
14th International Conference on Nuclear Engineering
July 17–20, 2006
Miami, Florida, USA
Conference Sponsors:
- Nuclear Engineering Division
ISBN:
0-7918-4245-2
PROCEEDINGS PAPER
CFD Simulation of 3D Flowfield in a Gas Centrifuge
Dongjun Jiang,
Dongjun Jiang
Tsinghua University, Beijing, China
Search for other works by this author on:
Shi Zeng
Shi Zeng
Tsinghua University, Beijing, China
Search for other works by this author on:
Dongjun Jiang
Tsinghua University, Beijing, China
Shi Zeng
Tsinghua University, Beijing, China
Paper No:
ICONE14-89783, pp. 403-408; 6 pages
Published Online:
September 17, 2008
Citation
Jiang, D, & Zeng, S. "CFD Simulation of 3D Flowfield in a Gas Centrifuge." Proceedings of the 14th International Conference on Nuclear Engineering. Volume 4: Computational Fluid Dynamics, Neutronics Methods and Coupled Codes; Student Paper Competition. Miami, Florida, USA. July 17–20, 2006. pp. 403-408. ASME. https://doi.org/10.1115/ICONE14-89783
Download citation file:
18
Views
Related Proceedings Papers
Related Articles
Self-Excited Oscillation of Transonic Flow Around an Airfoil in Two-Dimensional Channels
J. Turbomach (October,1990)
Numerical Investigation of Two-Phase Shock Waves in CO 2 Flows Using a Modified Hertz–Knudsen Model
J. Eng. Gas Turbines Power (March,2025)
Related Chapters
Aerodynamic Performance Analysis
Axial-Flow Compressors
Numerical Simulations of the Shockwave Induced Collapse of Bubbles Near Surfaces
Proceedings of the 10th International Symposium on Cavitation (CAV2018)
Definitions
Geometric Dimensioning and Tolerancing Handbook: Applications, Analysis & Measurement