An Investigation on the Geometric Effects of a Vertical-Downward Elbow on Two-Phase Flow

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An Investigation on the Geometric Effects of a Vertical-Downward Elbow on Two-Phase Flow Philip Graybill Grove City College Mechanical Engineering Andrew Hardison Robert Morris University Mechanical Engineering Advisor: Dr. Seungjin Kim Penn State University Mechanical and Nuclear Engineering July 30, 2015 Generously sponsored by the Toshiba-Westinghouse Fellows Program

This presentation investigates the geometric effects of a vertical-downward elbow on two-phase flow. Background Objective Single-Phase Flow CFD Modeling Two-Phase Flow Investigation

Researching geometric effects on two-phase flow can improve the safety of thermal-hydraulic reactor systems.

Geometry and pipe orientation dramatically affect two-phase flow. Port 4, L H = 3 D Port 7, L H = 93D j f = 1.5 m/s and j g,atm = 0.16 m/s Port 3, L VU = 60D Port 13, L VD = 67D Port 11, L VD = 3D

Flow Direction The experimental facility at Penn State enables data collection for a vertical-downward elbow. Width 29.5 ft. Vertical- Downward Elbow Water Test Section Height 10 ft. Elbow Radius = 6 in. Pipe Diameter = 2 in.

The experimental facility at Penn State enables data collection for a vertical-downward elbow. Combinatorial Test Facility Vertical-Downward Elbow

The objective of this research is to investigate the impacts of a vertical-downward elbow. Single-phase CFD analysis Establish Database Comparison Previous Studies Comparison

Single-phase flow in the facility was modeled with CFD to better understand the general elbow effects. Vertical-Upward Elbow Kim et al. (2014) Vertical-Downward Elbow 0D 3D 10D 50D

A turbulent secondary flow structure is created after the vertical-downard elbow. Incoming flow (r/r) P x (r/r) C y Inner wall z Outer wall

A secondary flow structure is created after the vertical-downard elbow. L=0D Incoming flow Streamwise Velocity

A secondary flow structure is created after the vertical-downard elbow. L=3D Incoming flow Streamwise Velocity

A secondary flow structure is created after the vertical-downard elbow. L=10D Incoming flow Streamwise Velocity

A secondary flow structure is created after the vertical-downard elbow. L=50D Incoming flow Streamwise Velocity

A secondary flow structure is created after the vertical-downard elbow. Progression Sequence L=0D Streamwise Velocity L=3D L=10D L=50D

A four-sensor conductivity probe collects local data as it moves across the pipe with a specialized measurement port.

A four-sensor conductivity probe collects local data as it moves across the pipe with a specialized measurement port. Incoming flow (r/r) P x inner wall (r/r) C 0 z y outer wall 120 data points/cross-section

New experimental data was collected at 0D and 3D after the vertical-downward elbow. Volumetric Flux (m/s) 5 4.5 4 3.5 3 2.5 2 1.5 1 0.5 0 New data collected for Run 7 & Run 8. Air Water Run 1 Run 2 Run 3 Run 4 Run 5 Run 6 Run 7 Run 8 0D 3D

Void fraction is measured with the conductivity probe in order to better understand two-phase flow structure. Void Fraction [-] Inner wall 0 ⁰ Outer wall 90 ⁰ 90.0 0.070 0.060 0.050 Run 7 J f : 4.00 m/s J g, atm : 0.23 m/s 0.040 0.030 0.020 0.010 0.000-1.0-0.8-0.6-0.4-0.2 0.0 0.2 0.4 0.6 0.8 1.0 r/r

Void fraction is measured with the conductivity probe in order to better understand two-phase flow structure. Void Fraction [-] Inner wall 0 ⁰ Run 7 J f : 4.00 m/s J g, atm : 0.23 m/s Outer wall 90 ⁰ 0.0 22.5 45.0 67.5 90.0 112.5 135.0 157.5 0.070 0.060 0.050 0.040 0.030 0.020 0.010 0.000-1.0-0.8-0.6-0.4-0.2 0.0 0.2 0.4 0.6 0.8 1.0 r/r

The void fraction distribution reveals a single peak after the vertical-downward elbow. L=0D L=3D Void Fraction Run 7 Volumetric liquid flux: 4.00 m/s Volumetric gas flux: 0.23 m/s

The void fraction distribution reveals a single peak after the vertical-downward elbow. L=0D L=3D Void Fraction Run 8 Volumetric liquid flux: 4.00 m/s Volumetric gas flux: 0.35 m/s

When compared, void fraction distribution and secondary flow show different flow characteristics. L=0D L=3D Void Fraction Single-phase CFD Velocity Two-phase Void Fraction data Run 7 Volumetric liquid flux: 4.00 m/s Volumetric gas flux: 0.23 m/s

When compared, void fraction distribution and secondary flow show different flow characteristics. L=0D L=3D Void Fraction Run 8 Volumetric liquid flux: 4.00 m/s Volumetric gas flux: 0.35 m/s

Swirling has a different impact after the vertical-downward elbow in comparison to the vertical-upward elbow. Incoming flow Vertical-Upward Elbow Vertical-Downward Elbow 3D 3D Run 4 Run 7

Swirling has a different impact after the vertical-downward elbow in comparison to the vertical-upward elbow. Incoming flow Vertical-Upward Elbow Vertical-Downward Elbow 3D 3D Single-phase CFD Velocity Two-phase Void Fraction data

Our reasearch provides new data and results for the verticaldownward elbow for future reactor safety. Single-phase CFD analysis Establish Database Comparison Previous Studies Comparison Questions?

ADDITIONAL SLIDES 22

Acknowledgements Special thanks to Toshiba Westinghouse for generously funding this Undergraduate Fellows Program. Lori Miraldi Lecturer in Communication Arts and Sciences Department of Communications Arts and Sciences The Pennsylvania State University lorimiraldi@psu.edu Dr. Seungjin Kim Associate Professor of Mechanical and Nuclear Engineering Department of Mechanical and Nuclear Engineering The Pennsylvania State University skim@psu.edu Shouxu Qiao Ph. D. Student The Pennsylvania State University szq105@psu.edu Questions?

Recommendations for future work Obtain more data for database of different flow rates and locations. Develop predictive models for two-phase flow around restrictions. Implement new models to reactor system analysis code for higher safety.

References A. Das, S.M. Ishtiaque, S.N. Singh, and A. Gupta, Optimization of fluid flow inside blowroom transport duct using CFD, Journal of the Textile Institute, pp. 1 12, 2014. Kim, S., Fu, X. Y., Wang, X., & Ishii, M. (2000). Development of the miniaturized four-sensor conductivity probe and the signal processing scheme. International Journal of Heat and Mass Transfer, 43(22), 4101-4118. doi:10.1016/s0017-9310(00)00046-6 Crawford, N. M., Cunningham, G., & Spence, S. W. T. (2007). An experimental investigation into the pressure drop for turbulent flow in 90 elbow bends. Proceedings of the Institution of Mechanical Engineers, Part E: Journal of Process Mechanical Engineering, 221(2), 77-88. doi:10.1243/0954408jpme84 Ishii, M., Hibiki, T., & SpringerLink (Online service). (2006). Thermo-fluid dynamics of two-phase flow. New York, N.Y: Springer Science+Business Media. Yadav, M. S., & Kim, S. (2013). Interfacial area transport across vertical elbows in air-water two-phase flow. Pennsylvania State University. University Park, Pa. Yadav, M., & Kim, S. (2013). EFFECTS OF 90-deg VERTICAL ELBOWS ON THE DISTRIBUTION OF LOCAL TWO- PHASE FLOW PARAMETERS. Nuclear Technology, 181(1), 94-105. Yadav, M., Worosz, T., Kim, S., Tien, K., & Bajorek, S. (2014). Characterization of the dissipation of elbow effects in bubbly two-phase flows. International Journal of Multiphase Flow, 66, 101-109. doi:10.1016/j.ijmultiphaseflow.2014.07.0 Kim, J., Yadav, M., & Kim, S. (2014). Characteristics of secondary flow induced by 90-degree elbow in turbulent pipe flow. Engineering Applications of Computational Fluid Mechanics, 8(2), 229-239. doi:10.1080/19942060.2014.11015509

This slide shows the measurement principle of the four-sensor conductivity probe. Measurement principle: conductivity difference between gas and liquid phases Impedance v i = Δs/Δt Downstream Sensor Upstream Sensor Δs Δt Time Local Time-Averaged a i (Ishii, 1975): a t i 1 1 T v n j i i j 23

The state-of-the-art four-sensory conductivity probe creates minimal distortion of bubbles. 4000 fps 24

These images show the size and configuration of the four-sensor conductivity probe. + V DC - V M DAQ 0.5 mm Path to ground through continuous phase Flow Acupuncture needle and 0.5 mm pencil lead

A mesh was generated for the loop geometry; this mesh was used as an input to the CFD solver. Accurate solutions require a well-constructed mesh. A mesh-sensitivity test confirmed that our results are grid-independent. 9

We have created high quality mesh to ensure accurate modeling Geometry accurately represents the test facility Structured O-mesh Units in mm 35

A mesh-sensitivity test demonstrates that our solution is gridindependent. Refinement Refinement 0.70 Million cells 3.02 Million cells 4.46 Million cells 29

The solution methods for our research compare well with previous research. Kim, J., Yadav, M., & Kim, S. (2014). Characteristics of secondary flow induced by 90-degree elbow in turbulent pipe flow. Software: OpenFOAM First Cell height: 20<Y + <50 Total Cell Number: 152,150 cells 37

Our results for the vertical-upward elbow were compared with previous research to confirm the accuracy of our simulations. ±5% Error Bars ±5% Error Bars 38

Secondary flow induced by elbow is seen to dissipate across nondimensional length through Swirl Intensity. Swirl Intensity (I s ) is defined as: Kim et al. (2014) correlation: where β=0.21 39

Dissipation Swirl Intensity measures the magnitude of secondary flow, which dissipates after an elbow. Swirl Intensity = Average Tangential Velocity Average Axial Velocity Cross Section with tangential velocity vectors 30

Swirl Intensity dissipates 90% by 15D after an elbow in CFX simulations. 90% dissipation 31

Swirl Intensity dissipates 90% by 15D after an elbow in CFX simulations. 90% dissipation 31

Swirl Intensity dissipation is independent of elbow orientation. 90% dissipation 32

The CFX simulations match the Swirl Intensity decay of OpenFOAM results. 44

CFD models were analyzed at 0D, 3D, 10D, and 50D after the vertical-downward elbow. 0D 3D 10D 10D 50D 4 m/s simulations 45

CFD models were analyzed at 0D, 3D, 10D, and 50D after the vertical-downward elbow. 0D 3D 10D 10D 50D 3 m/s simulations 46

CFD models were analyzed at 0D, 3D, 10D, and 50D after the vertical-downward elbow. 0D 3D 10D 10D 50D 2 m/s simulations 47

Pressure distribution changes at 0D, 1D, and 3D after the vertical-downward elbow (4m/s) 0D 8.6% absolute pressure difference 1D 2.0% absolute pressure difference 3D 1.3% absolute pressure difference 28

The area average void fraction and elbow strength of our data is comparable to previous research. Current Mena % Difference RUN 7 <α> [-] 0.047 0.066 28.8% σ [-] 0.4821 0.5638 14.5% RUN 5 <α> [-] 0.031 0.034 8.82 σ [-] 0.2464 0.2422 1.73 RUN 8 <α> [-] 0.046 0.05 8.00 σ [-] 0.2642 0.2585 2.21

The area average void fraction and elbow strength of our data is comparable to previous research. Run 7 3D Run 8 3D Run 5 3D New Data New Data New Data (Mena, 2015) (Mena, 2015) (Yadav, 2013)

OpenFoam simulations from Kim et al. (2014) agree closely with CFX results over entire elbow length. 51

Surface contours created from previous studies help better understand flow regime of the facility 25

Surface plots and Contour plots show void fractions from experiments. Incoming flow 3D Local Void Fraction (α) = time occupied by gas phase total time Repeat experiments, such as Run 5, confirm consistency with previous data. Run 5 Volumetric liquid flux: 3.00 m/s Volumetric gas flux: 0.23 m/s 15

The objective of this research is to investigate two-phase flow after a vertical-downward elbow. Bubbly Flow In Vertical Pipe Bubbly Flow In Vertical-Upward Elbow Flow rates and geometry dramatically change flow characteristics 54