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2/27/2023
ENGR:2510 Mechanics of Fluids and Transport Processes 2016F
1. Overview of Pipe Flow
2. CFD Process
3. ANSYS Workbench
4. ANSYS Design Modeler (Geometry)
5. ANSYS Mesh
6. ANSYS Fluent
6.1. Physics (Setup)
6.2. Solution
6.3. Results
2/27/2023 2
ENGR:2510 Mechanics of Fluids and Transport Processes 2016F
 Simulation of laminar pipe flow will be conducted
for this lab
 Axial velocity profile, centerline velocity, centerline
pressure, and wall shear stress will be analyzed
 Computational fluid dynamics (CFD) results for the
friction factor and the velocity profile will be
compared to analytical fluid dynamics (AFD)
 This lab will cover concept of laminar vs. turbulent
flow and developing length for pipe flows
Flow visualization between two parallel plates
(starts at 14:25)
2/27/2023 3
ENGR:2510 Mechanics of Fluids and Transport Processes 2016F
 Flow in pipe with Reynolds number (Re)
◦ 𝑅𝑒 =
𝑈𝐷
𝜈
=
𝐼𝑛𝑒𝑟𝑡𝑖𝑎𝑙 𝐹𝑜𝑟𝑐𝑒𝑠
𝑉𝑖𝑠𝑐𝑜𝑢𝑠 𝐹𝑜𝑟𝑐𝑒𝑠
where U is an inflow velocity, D is a diameter of pipe, 𝜈 is a kinematic viscosity
◦ Laminar : Re < 2300
◦ Turbulent : Re > 2300
 Differences between laminar and turbulent flow
◦ (mean) Velocity profile
◦ Pressure drop
◦ Developing length
◦ Wall shear stress and friction factor
Note: Refer to Chapter 8 of your book for more details
Flow visualization of transition from laminar to turbulent flow
2/27/2023 4
ENGR:2510 Mechanics of Fluids and Transport Processes 2016F
 The overall procedure for simulation of pipe flow is shown on chart below
 Although we will be making the mesh before we define the physics you have to know the
physics to design appropriate mesh.
Geometry Physics Mesh Solution Results
Pipe (ANSYS
Design Modeler)
Structure
(ANSYS Mesh)
Uniform
(ANSYS Mesh)
General (ANSYS
Fluent - Setup)
Model (ANSYS
Fluent - Setup)
Boundary
Conditions
(ANSYS Fluent
-Setup)
Reference
Values
(ANSYS Fluent
- Setup)
Laminar
Solution
Methods
(ANSYS Fluent
- Solution)
Monitors
(ANSYS Fluent
- Solution)
Solution
Initialization
(ANSYS Fluent
-Solution)
Plots (ANSYS
Fluent- Results)
Graphics and
Animations
(ANSYS
Fluent- Results)
2/27/2023 5
ENGR:2510 Mechanics of Fluids and Transport Processes 2016F
 Design your simulation using ANSYS Workbench
ANSYS Design Modeler
(Geometry)
ANSYS Mesh
(Mesh)
ANSYS Fluent
(Physics, Solution and Results)
2/27/2023 6
ENGR:2510 Mechanics of Fluids and Transport Processes 2016F
Parameter Value
Radius of pipe, R 0.02619 m
Diameter of pipe, D 0.05238 m
Length of pipe, L 7.62 m
L
R
D
 Symmetric property of the flow is used to
create 2D representation of the 3D pipe flow
Inlet Outlet
Wall
Center
Flow
2/27/2023 7
ENGR:2510 Mechanics of Fluids and Transport Processes 2016F
 Create uniform grid distribution (for laminar flow, Pre-lab 1)
2/27/2023 8
ENGR:2510 Mechanics of Fluids and Transport Processes 2016F
 Using ANSYS fluent define physics of the flow, solve CFD simulation and analyze results
Physics (Setup) Solution Results
2/27/2023 9
ENGR:2510 Mechanics of Fluids and Transport Processes 2016F
 Laminar flow
 Air properties
 Boundary Conditions (BC)
◦ No-slip: velocities and pressure gradient is zero (𝑣𝑥 = 0, 𝑣𝑟 = 0,
𝑑𝑝
𝑑𝑟
= 0)
◦ Symmetric: radial velocity and gradients of axial velocity and pressure are zero (
𝑑𝑣𝑥
𝑑𝑟
= 0, 𝑣𝑟 = 0,
𝑑𝑝
𝑑𝑟
= 0)
◦ Inlet velocity: uniform constant velocity (𝑣𝑥 = 0.2 [𝑚/𝑠], 𝑣𝑟 = 0,
𝑑𝑝
𝑑𝑟
= 0)
◦ Outlet: (gauge) pressure is imposed to the boundary (
𝑑𝑣𝑥
𝑑𝑥
= 0,
𝑑𝑣𝑟
𝑑𝑥
= 0, 𝑝 = 𝑝𝑔𝑎𝑢𝑔𝑒 = 0 (𝑓𝑜𝑟 𝑃𝑟𝑒𝑙𝑎𝑏1))
Inlet – Velocity inlet BC Outlet – Pressure outlet BC
Wall – No slip BC
Center – Axisymmetric BC
Flow
Zero slop at center or
𝑑𝑣𝑥
𝑑𝑟
= 0
r
x
2/27/2023 10
ENGR:2510 Mechanics of Fluids and Transport Processes 2016F
 A limiting behavior in the solution of the equations
 Represented by the history of residuals or errors made by previous iterative solutions
 A converged solution is not necessarily an accurate one due to iteration number, domain size,
mesh resolution and numerical schemes
 Continuity, momentum equation have their own residual histories
2/27/2023 11
ENGR:2510 Mechanics of Fluids and Transport Processes 2016F
 Developed length is distance from entrance to a point where
flow is fully developed
 Fully developed flow does not change velocity profile or velocity
gradient in axial direction is zero
 Pressure drops linearly
 Axial velocity or skin friction distribution along axis can be used
to determine the length
Developing
region
Developed
region
2/27/2023 12
ENGR:2510 Mechanics of Fluids and Transport Processes 2016F
 Flow can be visualized in detail by using CFD
2/27/2023 13
ENGR:2510 Mechanics of Fluids and Transport Processes 2016F
 Bring your EFD 2 Data Reduction Sheet for the CFD Lab 1 by next week
 Deadline for the CFD Lab 1 report is two weeks after from your CFD lab 1 (not Pre-lab 1)
 Use the Lab drop-box when turning in your lab reports
 Come to the office hours for any help
2/27/2023 14

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Intro_Pre-Lab1.pptx

  • 2. ENGR:2510 Mechanics of Fluids and Transport Processes 2016F 1. Overview of Pipe Flow 2. CFD Process 3. ANSYS Workbench 4. ANSYS Design Modeler (Geometry) 5. ANSYS Mesh 6. ANSYS Fluent 6.1. Physics (Setup) 6.2. Solution 6.3. Results 2/27/2023 2
  • 3. ENGR:2510 Mechanics of Fluids and Transport Processes 2016F  Simulation of laminar pipe flow will be conducted for this lab  Axial velocity profile, centerline velocity, centerline pressure, and wall shear stress will be analyzed  Computational fluid dynamics (CFD) results for the friction factor and the velocity profile will be compared to analytical fluid dynamics (AFD)  This lab will cover concept of laminar vs. turbulent flow and developing length for pipe flows Flow visualization between two parallel plates (starts at 14:25) 2/27/2023 3
  • 4. ENGR:2510 Mechanics of Fluids and Transport Processes 2016F  Flow in pipe with Reynolds number (Re) ◦ 𝑅𝑒 = 𝑈𝐷 𝜈 = 𝐼𝑛𝑒𝑟𝑡𝑖𝑎𝑙 𝐹𝑜𝑟𝑐𝑒𝑠 𝑉𝑖𝑠𝑐𝑜𝑢𝑠 𝐹𝑜𝑟𝑐𝑒𝑠 where U is an inflow velocity, D is a diameter of pipe, 𝜈 is a kinematic viscosity ◦ Laminar : Re < 2300 ◦ Turbulent : Re > 2300  Differences between laminar and turbulent flow ◦ (mean) Velocity profile ◦ Pressure drop ◦ Developing length ◦ Wall shear stress and friction factor Note: Refer to Chapter 8 of your book for more details Flow visualization of transition from laminar to turbulent flow 2/27/2023 4
  • 5. ENGR:2510 Mechanics of Fluids and Transport Processes 2016F  The overall procedure for simulation of pipe flow is shown on chart below  Although we will be making the mesh before we define the physics you have to know the physics to design appropriate mesh. Geometry Physics Mesh Solution Results Pipe (ANSYS Design Modeler) Structure (ANSYS Mesh) Uniform (ANSYS Mesh) General (ANSYS Fluent - Setup) Model (ANSYS Fluent - Setup) Boundary Conditions (ANSYS Fluent -Setup) Reference Values (ANSYS Fluent - Setup) Laminar Solution Methods (ANSYS Fluent - Solution) Monitors (ANSYS Fluent - Solution) Solution Initialization (ANSYS Fluent -Solution) Plots (ANSYS Fluent- Results) Graphics and Animations (ANSYS Fluent- Results) 2/27/2023 5
  • 6. ENGR:2510 Mechanics of Fluids and Transport Processes 2016F  Design your simulation using ANSYS Workbench ANSYS Design Modeler (Geometry) ANSYS Mesh (Mesh) ANSYS Fluent (Physics, Solution and Results) 2/27/2023 6
  • 7. ENGR:2510 Mechanics of Fluids and Transport Processes 2016F Parameter Value Radius of pipe, R 0.02619 m Diameter of pipe, D 0.05238 m Length of pipe, L 7.62 m L R D  Symmetric property of the flow is used to create 2D representation of the 3D pipe flow Inlet Outlet Wall Center Flow 2/27/2023 7
  • 8. ENGR:2510 Mechanics of Fluids and Transport Processes 2016F  Create uniform grid distribution (for laminar flow, Pre-lab 1) 2/27/2023 8
  • 9. ENGR:2510 Mechanics of Fluids and Transport Processes 2016F  Using ANSYS fluent define physics of the flow, solve CFD simulation and analyze results Physics (Setup) Solution Results 2/27/2023 9
  • 10. ENGR:2510 Mechanics of Fluids and Transport Processes 2016F  Laminar flow  Air properties  Boundary Conditions (BC) ◦ No-slip: velocities and pressure gradient is zero (𝑣𝑥 = 0, 𝑣𝑟 = 0, 𝑑𝑝 𝑑𝑟 = 0) ◦ Symmetric: radial velocity and gradients of axial velocity and pressure are zero ( 𝑑𝑣𝑥 𝑑𝑟 = 0, 𝑣𝑟 = 0, 𝑑𝑝 𝑑𝑟 = 0) ◦ Inlet velocity: uniform constant velocity (𝑣𝑥 = 0.2 [𝑚/𝑠], 𝑣𝑟 = 0, 𝑑𝑝 𝑑𝑟 = 0) ◦ Outlet: (gauge) pressure is imposed to the boundary ( 𝑑𝑣𝑥 𝑑𝑥 = 0, 𝑑𝑣𝑟 𝑑𝑥 = 0, 𝑝 = 𝑝𝑔𝑎𝑢𝑔𝑒 = 0 (𝑓𝑜𝑟 𝑃𝑟𝑒𝑙𝑎𝑏1)) Inlet – Velocity inlet BC Outlet – Pressure outlet BC Wall – No slip BC Center – Axisymmetric BC Flow Zero slop at center or 𝑑𝑣𝑥 𝑑𝑟 = 0 r x 2/27/2023 10
  • 11. ENGR:2510 Mechanics of Fluids and Transport Processes 2016F  A limiting behavior in the solution of the equations  Represented by the history of residuals or errors made by previous iterative solutions  A converged solution is not necessarily an accurate one due to iteration number, domain size, mesh resolution and numerical schemes  Continuity, momentum equation have their own residual histories 2/27/2023 11
  • 12. ENGR:2510 Mechanics of Fluids and Transport Processes 2016F  Developed length is distance from entrance to a point where flow is fully developed  Fully developed flow does not change velocity profile or velocity gradient in axial direction is zero  Pressure drops linearly  Axial velocity or skin friction distribution along axis can be used to determine the length Developing region Developed region 2/27/2023 12
  • 13. ENGR:2510 Mechanics of Fluids and Transport Processes 2016F  Flow can be visualized in detail by using CFD 2/27/2023 13
  • 14. ENGR:2510 Mechanics of Fluids and Transport Processes 2016F  Bring your EFD 2 Data Reduction Sheet for the CFD Lab 1 by next week  Deadline for the CFD Lab 1 report is two weeks after from your CFD lab 1 (not Pre-lab 1)  Use the Lab drop-box when turning in your lab reports  Come to the office hours for any help 2/27/2023 14

Editor's Notes

  1. Introduce yourself Introduce Lab – Simulation of Laminar Pipe Flow in smooth pipe
  2. Questions: What is the velocity at the wall? Talking Points: Simulating laminar pipe flow Comparing CFD results to AFD solutions Look at the developing profile Uniform inlet to quadratic Linear pressure drop in fully developed flow Developing length
  3. Talking Points: Laminar flow is viscous dominated Low Re # Turbulent flow is inertial dominated High Re #
  4. Talking Points: Physics must be known to properly construct mesh/grid Example: must know if flow is turbulent to determine grid refinement for B.L. Need many grid points to resolve large velocity grads noticed in turbulent B.L. In ANSYS mesh comes before physics
  5. Talking Points: ANSYS Workbench Project Schematic screen Modular interface Geometry-> Mesh-> Physics-> Solution->Results
  6. Talking Points: In CFD it is best to simplify problem for efficiency Pipe can be simplified into 2D rectangle axisymmetric about centerline
  7. Talking Points: CFD is discretizing the fluid flow and solving N.S. eqns numerically at each grid point Discretize geometry by splitting sides Can get information at any discretized point
  8. Talking Points: User interface of Fluent Physics (Setup) Solution Numerical methods setup Results
  9. Talking Points: No slip wall Symmetric about axis for axial velocity and pressure Uniform inlet velocity Outlet pressure
  10. Talking Points: Residuals are relative errors, taking the difference between the previous solution and current solution Just because residuals go to zero does not mean solution is perfectly accurate May be converging to the wrong solution Dependent on many factors such as turbulence modeling
  11. Questions: Can anyone explain what fully developed flow is? Why is friction coefficient constant in fully developed Talking Points: Explain developing length Linear pressure drop in fully developed
  12. Questions: What happens to radial velocity in developed region? Talking Points: Shows contours of axial velocity Vectors of axial velocity CFD allows you to find fluid properties at any point in the fluid domain