Page History

Author:

Rajesh

Bhaskaran,

Cornell University

Problem Specification
1. Create Geometry in GAMBIT
2. Mesh Geometry in GAMBIT
3. Specify Boundary Types in GAMBIT
4. Set Up Problem in FLUENT
5. Solve!
6. Analyze Results
7. Refine Mesh
Problem 1
Problem 2

 University

{color:#ff0000}{*}Problem Specification{*}{color}
[1. Create Geometry in GAMBIT|Laminar Pipe Flow - Pre-Analysis & Start-Up]
[2. Mesh Geometry in GAMBIT|Laminar Pipe Flow - Geometry]
[3. Specify Boundary Types in GAMBIT|Laminar Pipe Flow - Mesh]
[4. Set Up Problem in FLUENT|FLUENT - Laminar Pipe Flow Step 4]
[5. Solve\!|FLUENT - Laminar Pipe Flow Step 5]
[6. Analyze Results|FLUENT - Laminar Pipe Flow Step 6]
[7. Refine Mesh|FLUENT - Laminar Pipe Flow - Verification & Validation]
[Problem 1|FLUENT - Laminar Pipe Flow - Exercises]
[Problem 2|FLUENT - Laminar Pipe Flow - Problem 2]
{panel}

h2. Problem Specification

!Fluent_pipeflow.jpg|width=32,height=32!

Consider fluid flowing through a circular pipe of constant cross-section. The pipe diameter _D_ = 0.2 m and length _L_ = 8 m. The inlet velocity _Ū{_}{_}{~}z{~}_ = 1 m/s. Consider the velocity to be constant over the inlet cross-section. The fluid exhausts into the ambient atmosphere which is at a pressure of 1 atm. Take density _ρ = 1 kg/ m{_}{_}{^}3{^}_ and coefficient         of viscosity _µ = 2 x 10{_}{_}^\-3{^}_ _kg/(ms)._ The Reynolds number _Re_ based on the pipe diameter is
{latex}
\large
$$
{Re} = {\rho {\bar{U}}_zD \over \mu} = 100
$$
{latex}
where _Ū{_}{_}{~}z{~}_ is the average velocity at the inlet, which is 1 m/s in this case.

Solve this problem using FLUENT. Plot the centerline velocity, wall         skin-friction coefficient, and velocity profile at the outlet. Validate         your results.

Note: The values used for the inlet velocity and flow properties are         chosen for convenience rather than to reflect reality. The key parameter         value to focus on is the Reynolds no.

h2. Preliminary Analysis

We expect the viscous boundary layer to grow along the pipe starting         at the inlet. It will eventually grow to fill the pipe completely (provided         that the pipe is long enough). When this happens, the flow becomes fully-developed         and there is no variation of the velocity profile in the axial direction, _x_ (see         figure below). One can obtain a closed-form solution to the governing         equations in the fully-developed region. You should have seen this in         the _Introduction to Fluid Mechanics_ course. We will compare the         numerical results in the fully-developed region with the corresponding         analytical results. So it's a good idea for you to go back to your textbook         in the Intro course and review the fully-developed flow analysis. What         are the values of centerline velocity and friction factor you expect         in the fully-developed region based on the analytical solution? What         is the solution for the velocity profile?

!TurbulentPipe.jpg|width=32,height=32!

We'll create the geometry and mesh in GAMBIT which is the preprocessor         for FLUENT, and then read the mesh into FLUENT and solve for the flow         solution.

Go to [Step 1: Create Geometry in GAMBIT|Laminar Pipe Flow - Pre-Analysis & Start-Up]

[See and rate the complete Learning Module|FLUENT - Laminar Pipe Flow]

[Go to all FLUENT Learning Modules|FLUENT Learning Modules]