11th International Conference on Mechanical Engineering (ICME2015)

Slides:



Advertisements
Similar presentations
A mathematical model of steady-state cavitation in Diesel injectors S. Martynov, D. Mason, M. Heikal, S. Sazhin Internal Engine Combustion Group School.
Advertisements

PHOENICS Based Arc Models as a Test Tool
Introduction Acoustic radiation forces on particles within standing waves are used in processes such as particle separation, fractionation and agglomeration.
Open Source Field Operation and Manipulation
1 Application of for Predicting Indoor Airflow and Thermal Comfort.
Dominic Hudson, Simon Lewis, Stephen Turnock
University of Minho School of Engineering Uma Escola a Reinventar o Futuro – Semana da Escola de Engenharia - 24 a 27 de Outubro de 2011 Abstract The inherent.
Usefulness of velocity profiles based on 3D cine PC MR used as boundary conditions for computational fluid dynamics of an intracranial aneurysm : investigation.
CHAPTER 5: Mass and Energy Analysis of Control Volumes
The Flame Deflector and Five Segment Booster By: Geoffrey Husk.
T. YOSHIDA, J. OYAMA, T. HIGUCHI, T. ABE and T. HIRAYAMA Department of Electrical and Electronic Engineering, Nagasaki University, Japan ON THE CHARACTERISTICS.
C OMPUTATIONAL F LUID D YNAMIC M ODEL OF A RTERIOVENOUS F ISTULA A NASTOMOSIS TO S TUDY THE E FFECTS OF V ESSEL S IZE AND P RESSURE G RADIENT ON THE P.
Experimental and Numerical Study of the Effect of Geometric Parameters on Liquid Single-Phase Pressure Drop in Micro- Scale Pin-Fin Arrays Valerie Pezzullo,
Fluid Mechanics –For Civil Engineers is all about SMU Storing– Moving– Using ( Incompressible fluids - water) To design and manage these systems we need.
Mark Claywell & Donald Horkheimer University of Minnesota
Thermo-fluid Analysis of Helium cooling solutions for the HCCB TBM Presented By: Manmeet Narula Alice Ying, Manmeet Narula, Ryan Hunt and M. Abdou ITER.
Engineering H191 - Drafting / CAD The Ohio State University Gateway Engineering Education Coalition Lab 4P. 1Autumn Quarter Transport Phenomena Lab 4.
Thermal Analysis of Helium- Cooled T-tube Divertor S. Shin, S. I. Abdel-Khalik, and M. Yoda ARIES Meeting, Madison (June 14-15, 2005) G. W. Woodruff School.
MECH 221 FLUID MECHANICS (Fall 06/07) Chapter 9: FLOWS IN PIPE
Tony Y. Bougebrayel, PE, PhD
Chamber Dynamic Response Modeling Zoran Dragojlovic.
University of South Carolina FCR Laboratory Dept. of Chemical Engineering By W. K. Lee, S. Shimpalee, J. Glandt and J. W. Van Zee Fuel Cell Research Laboratory.
PHAROS UNIVERSITY ME 259 FLUID MECHANICS FOR ELECTRICAL STUDENTS Basic Equations for a Control Volume.
Simulation of Droplet Drawback in Inkjet Printing
ICHS4, San Francisco, September E. Papanikolaou, D. Baraldi Joint Research Centre - Institute for Energy and Transport
Department of Flow, Heat and Combustion Mechanics – Ghent University – UGent Linear stability analysis of a supercritical loop C.
© 2011 Autodesk Freely licensed for use by educational institutions. Reuse and changes require a note indicating that content has been modified from the.
Thermal Model of MEMS Thruster Apurva Varia Propulsion Branch Code 597.
1 Department: Material science and engineering Discipline: Finite element method By: Anelia Ivanova To: Prof. V. Iliev Subject : Hydrodynamics Simulation.
Page 1 SIMULATIONS OF HYDROGEN RELEASES FROM STORAGE TANKS: DISPERSION AND CONSEQUENCES OF IGNITION By Benjamin Angers 1, Ahmed Hourri 1 and Pierre Bénard.
CHAPTER 5: Mass and Energy Analysis of Control Volumes
ChemE 260 Conservation of Mass & Energy, Steady-State Processes April 15, 2005 Dr. William Baratuci Senior Lecturer Chemical Engineering Department University.
Mass Transfer Coefficient
Department Of Material Science And Engineering FINITE ELEMENT METHOD UNIVERSITY OF CHEMICAL TECHNOLOGY AND METALLURGY Sofia Nina Velikova, June 2010.
Computational Fluid Dynamics Applied to the Analysis of 10-mm Hydrocyclone Solids Separation Performance S. A. Grady, M. M. Abdullah, and G. D. Wesson.
Numerical simulation of droplet motion and two-phase flow field in an oscillating container Tadashi Watanabe Center for Computational Science and e-Systems.
Department of Mechanical Engineering, IUPUI Christina Koehly Michael Schneider Internship Students from Germany Indiana University - Purdue University.
PRESENTATION OF CFD ACTIVITIES IN CV GROUP Daniel Gasser.
CFD Study of the Development of Vortices on a Ring Wing
Lecture Objectives: Define 1) Reynolds stresses and
CFD Simulation Investigation of Natural Gas Components through a Drilling Pipe RASEL A SULTAN HOUSSEMEDDINE LEULMI.
Date of download: 9/26/2017 Copyright © ASME. All rights reserved.
CFD ANALYSIS OF MULTIPHASE TRANSIENT FLOW IN A CFB RISER
From: Hydraulic Loss of Finite Length Dividing Junctions
Novel Simulation Model for GM type Orifice Pulse Tube Cryocooler
Hamdache Abderrazaq 1*, Belkacem Mohamed 1, Hannoun Nourredine 2
4th Global Engineering, Science and Technology Conference
Chapter: 06 MASS AND ENERGY ANALYSIS OF CONTROL VOLUMES.
Titolo presentazione sottotitolo
MASS AND ENERGY ANALYSIS OF CONTROL VOLUMES
GANIL-SPIRAL2 DESIGN OFFICE MECHANiCAL SIMULATION WITH
Mass and Energy Analysis of Control Volumes
Prepared BY: Helwan University Faculty Of Engineering
Basics of Fuel Injection in Ports
Flow Through a Pipe Elbow (Comsol)
Multi-physics Simulation of a Wind Piezoelectric Energy Harvester Validated by Experimental Results Giuseppe Acciani, Filomena Di Modugno, Ernesto Mininno,
Chapter 4. Analysis of Flows in Pipes
Lecture Objectives Learn about Implementation of Boundary Conditions
Title J. A. Smith1, M. B. Fields2
Space Distribution of Spray Injected Fluid
Comparison between Serrated & Notched Serrated Heat Exchanger Fin Performance Presented by NABILA RUBAIYA.
Title J. A. Smith1, M. B. Fields2
Title J. A. Smith, M. B. Fields2
Title J. A. Smith1, M. B. Fields2
E. Papanikolaou, D. Baraldi
Lecture Objectives: Boundary Conditions Project 1 (software)
Lecture Objectives: Start using CFD Software Class project 1
Title J. A. Smith1, M. B. Fields2
Ch. 4 The first law of thermodynamics: Control Volume
PANDA Collaboration Meeting
Presentation transcript:

11th International Conference on Mechanical Engineering (ICME2015) Paper ID: 502 Effects of Flow Properties on the Performance of a Diffuser-Nozzle Element of a Valveless Micropump Authors: Partha Kumar Das A.B.M. Toufique Hasan Department of Mechanical Engineering Bangladesh University of Engineering & Technology (BUET)

Objective To study the flow behaviour through a diffuser-nozzle element of a valveless micropump To process the performance parameters(rectification capability, energy loss, etc) of diffuser-nozzle element To simulate the performance of diffuser-nozzle element for different boundary conditions To compare the performance of diffuser-nozzle element for different conditions and its compatibility for different applications

Micropump specialized microfluidic device a length scale in micrometer range both small scale flow (usually less than 30 μL/min) high pressure fluid transport .

Micropump Classification Mechanical Displacement Micropump Piezoelectric Thermopneumatic Electrostatic Bimetallic Electromagnetic Acoustic Standing Wave Micropump (ASWMP) Dynamic Micropump Magnetohydrodynamic (MHD Electrohydrodynamic (EHD) Electroosmotic Application of Micropumps Micropump has found a wide range applications in different fields like- Biofluidic and Microfluidic Field Chemical and Biological Sample Analysis Electronic Cooling in Micro Integrated Circuits (µ-IC)

Acoustic Standing Wave Micropump: The youngest micropump in literature

Valves vs. Diffuser-nozzle Element Dynamic Effect of Flow in a diffuser-nozzle element: causes a greater flow resistance in nozzle direction than in diffuser direction for the same pressure difference As a result a net flow is achieved through outlet port.

Geometry of the Present Work A planar, 2-D diffuser-nozzle element has been used Inlet length: 0.2 mm in x-direction Inlet height from symmetry line: 0.06 mm in y-direction Diffuser-nozzle section: 1.2 mm in x-direction Outlet length: 0.2 mm in x-direction Outlet height from symmetry line:1.26 mm in y-direction

2-D Meshing A hybrid meshing has been used with structured mesh in inlet and outlet region and unstructured mesh in main diffuser-nozzle section. Total no. of cells varies from 30000 to 40000.

3-D Meshing Span in z direction: 1mm Total No. of cells: 427910 12226 Cells in 2D 35 Cells along 1 mm Span

Numerical Procedures ANSYS Fluent pressure based solver (based on Finite Volume Method) has been used for the simulation process with the following conditions- Planer 2D space, Laminar, Transient flow Working Fluid: Water (Density=998.2 kg/m3, viscosity=0.001003 kg/ m.s) Boundary Conditions: Operating condition=101325 Pa Pressure-Inlet: sinusoidal pressure inlet, P(t) = P sin(ωt) Pressure-Outlet: zero pressure outlet Symmetry Boundary Condition in planer boundary Number of Time Step per Cycle: 200 The post-processing is done on TECPLOT software

Governing Equations Conservation of Mass Conservation of Momentum (Navier-Stokes Equation)

Diffuser Efficiency (η) Diffuser efficiency is one of the most important performance parameter indicating the net flow rate through diffuser-nozzle element. where, εn and εd are the flow resistance or pressure loss coefficients of the nozzle and diffuser direction respectively. Rectification Capability The capability of a diffuser-nozzle element to direct the flow in a definite direction. Higher the rectification capability higher amount of flow towards diffuser direction lower backflow towards nozzle direction Rectification Capability , ξ= ∅ + − ∅ − ∅ + + ∅ − Ø+ total volume flow in the diffuser direction ∅ + Ø- total volume flow in the nozzle direction ∅ −

Validation with Reference Paper Frequency: 10 kHz, Peak Pressure: 10 kPa Reference: Nabavi, M. and L. Mongeau (2009). "Numerical analysis of high frequency pulsating flows through a diffuser-nozzle element in valveless acoustic micropumps." Microfluidics and Nanofluidics 7(5): 669-681.

Justification of 2-D assumption with 3-D model

Stream Function Contour for 2-D Model Peak Pressure: 10 kPa, Frequency: 10 kHz, Inlet length / Outlet length: 0.2 mm / 0.2 mm α =9°° α =0°° (b) (a) α =45°° (c) α : Phase angle α =68.4°° (a) α =72°° (b)

Stream Function Contour for 2-D Model (b) α =85°° α =80°° (a) (d) α =255°° α =171.5°°

Stream Function Contour for 2-D Model (b) α =260°° α =262°° (c) α =265°°

Stream Function Contour for 2-D Model (b) α =269°° α =266°° (c) α =270°°

Stream Function Contour for 2-D Model (b) α =273°° α =271°° (c) α =275°°

Stream Function Contour for 2-D Model (b) α =281°° α =279°° (c) (d) α =288°° α =295°°

Stream Function Contour for 2-D Model (b) α =325°° α =300°° (c) α =358°°

Driving Frequency (kHz) Comparison of Performance Parameters Peak Pressure = 10 kPa Driving Frequency (kHz) 5 10 20 30 50 Net Velocity (mm/min) 8922 3156 1336 423 252 Net Volume Flow Rate (mL/min) 1.07065 0.3786 0.1603 0.05076 0.03024 Rectification Capability , ξ= 32.01% 22.34% 19.33% 10.02% 9.2% Diffuser Efficiency, η= 2.149 1.726 1.62 1.2731 1.279

Conclusion The asymmetry of velocity wave represents a net flow in diffuser direction Flow circulation occurs at the peak positive and negative pressure region. With increase in frequency, diffuser-nozzle element becomes ineffective in flow rectification.

THANK YOU ?

Appendix Calculation procedures of performance parameters of diffuser-nozzle element for 50 kHz

Fig.A5 Total pressure difference between inlet2 and outlet2