Relaxation Techniques in Computational Fluid Dynamics

 
Relaxation Technique
CFD
 
Dr. Ugur GUVEN
 
Elliptic Partial Differential Equations
 
Elliptic Partial Differential Equations are particularly
useful for analyzing fluid flow that change upstream
as well as downstream.
The most famous of these equations if the Laplace
Equation.
Laplace Equation is used to give the velocity
potential of inviscid incompressible irrotational flow
 
Solution by the Relaxation Method
 
Now you rewrite the Laplace Equation in terms of
second order central differences.
 
Grid for the Relaxation Technique
 
Relaxation Technique
 
Iterative Steps
 
Rewrite the equation obtained in the previous slide
to solve for n+1 which is the number of iterations.
Note that this is different form time marching
technique as the flow variables don’t change over
time, but they change over distance. (REMEMBER
THE EQUATION DOESN’T HAVE dt TERMS)
 
Iteration Steps
 
1 ) We already know the boundary values from 1 to 20, so we
will use those.
2) Assume some value for the remaining 15 points.
3) Use the equation to solve for each 15 points.
 
Examples of the Iteration Steps
 
Since we already have fixed boundary values
for nodes 1-20, lets apply the equation to
node 21 for value n+1. 
(Remember we
assumed values for the first step n=1)
 
Next Step
 
Now, when we are calculating Node 22, we can use
the value from Node 21 that was calculated one
step ago for better accuracy.
Do this for each of the 15 nodes in the grid.
 
Summary of Relaxation Technique
 
We continue to do this for every node until all
15 nodes have been written and calculated for
a single iteration.
Repeat these steps for as many iterations as
possible (minimum 10) for more accurate
results.
Use calculated results in your new node
calculations whenever possible.
 
Thank You
 
 
 
You can download this lecture at
 
www.cfdlectures.co.cc
 
drguven@live.com
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This content delves into the application of relaxation techniques in Computational Fluid Dynamics, focusing on the analysis of fluid flow using Elliptic Partial Differential Equations. It explains the iterative steps involved in solving equations through relaxation methods for accurate results.

  • Computational Fluid Dynamics
  • Relaxation Techniques
  • Fluid Flow Analysis
  • Iterative Methods
  • Elliptic Equations

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  1. Relaxation Technique CFD Dr. Ugur GUVEN

  2. Elliptic Partial Differential Equations Elliptic Partial Differential Equations are particularly useful for analyzing fluid flow that change upstream as well as downstream. The most famous of these equations if the Laplace Equation. Laplace Equation is used to give the velocity potential of inviscid incompressible irrotational flow

  3. Solution by the Relaxation Method Now you rewrite the Laplace Equation in terms of second order central differences.

  4. Grid for the Relaxation Technique

  5. Relaxation Technique

  6. Iterative Steps Rewrite the equation obtained in the previous slide to solve for n+1 which is the number of iterations. Note that this is different form time marching technique as the flow variables don t change over time, but they change over distance. (REMEMBER THE EQUATION DOESN T HAVE dt TERMS)

  7. Iteration Steps 1 ) We already know the boundary values from 1 to 20, so we will use those. 2) Assume some value for the remaining 15 points. 3) Use the equation to solve for each 15 points.

  8. Examples of the Iteration Steps Since we already have fixed boundary values for nodes 1-20, lets apply the equation to node 21 for value n+1. (Remember we assumed values for the first step n=1)

  9. Next Step Now, when we are calculating Node 22, we can use the value from Node 21 that was calculated one step ago for better accuracy. Do this for each of the 15 nodes in the grid.

  10. Summary of Relaxation Technique We continue to do this for every node until all 15 nodes have been written and calculated for a single iteration. Repeat these steps for as many iterations as possible (minimum 10) for more accurate results. Use calculated results in your new node calculations whenever possible.

  11. Thank You You can download this lecture at www.cfdlectures.co.cc drguven@live.com

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