Computational Fluid Dynamics Applied to the Analysis of 10-mm Hydrocyclone Solids Separation Performance - PowerPoint PPT Presentation

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Computational Fluid Dynamics Applied to the Analysis of 10-mm Hydrocyclone Solids Separation Performance

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S. A. Grady, M. M. Abdullah, and G. D. Wesson. Department of Chemical Engineering. Florida A&M University/Florida State University College of Engineering ... – PowerPoint PPT presentation

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Title: Computational Fluid Dynamics Applied to the Analysis of 10-mm Hydrocyclone Solids Separation Performance


1
Computational Fluid Dynamics Applied to the
Analysis of 10-mm Hydrocyclone Solids Separation
Performance
  • S. A. Grady, M. M. Abdullah, and G. D. Wesson

Department of Chemical Engineering Florida AM
University/Florida State University College of
Engineering
2
Presentation Outline
  • Research Objectives
  • Experimental Procedures
  • Solution Details Results
  • Conclusions
  • Continued Work
  • Acknowledgments

3
Research Objectives
  • Develop Flow Field Predictions for Reynolds
    Stress Turbulence Model
  • Comparison of Flow Field Properties for Different
    Geometries
  • Validate Flow Field Prediction
  • Solid Particle Motion
  • Apply Drop Break-up Model with Separation for
    Liquid/Liquid Systems

4
Experimental Procedure
  • 10-mm Geometry
  • Develop Grid
  • Establish Boundary Conditions
  • Perform RSM Simulation Using FLUENT
  • Identify Appropriate Flow Structures

5
3-D Cyclone Grid
Tangential Inlet Configuration
Volute Inlet Configuration
6
Grid Information
  • Tangential Inlet
  • Hexahedral and Tetrahedral Cells
  • 532,863 cells
  • 1,095,577 faces
  • Volute Inlet
  • Hexahedral Cell Type
  • 175,506 cells
  • 544,937faces

7
Boundary Conditions
  • Flow Split
  • Inlet Volumetric Flow Rate
  • Plug flow profile normal to inlet face

8
Results
Velocity profiles Velocity vectors Core properties
9
Axial Velocity Profiles
10
Tangential Velocity Profiles
11
Velocity Vectors
Volute Inlet Configuration
Tangential Inlet Configuration
12
Turbulence Intensity
13
Pressure Distribution
14
Locus of Zero Axial Velocity
15
Locus of Zero Tangential Velocity
16
Conclusions
  • Volute Inlet Configuration Provides
  • Greater symmetry about the axis of symmetry
  • Lower turbulence intensity
  • Reynolds Stress Model Predictions Provide

17
Continued Work
  • Model Validation Based on Separation Principles
  • Particle migration analysis
  • Turbulence intensity based drop break-up analysis
  • Model Validation Based on LDV Experiments

18
Acknowledgements
FAMU/NASA Graduate Fellowship Program Florida AM
University Foundation
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