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  • FLUENT - Compressible Flow in a Nozzle- Step 6 *New

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Author: Rajesh Bhaskaran & Yong Sheng Khoo, Cornell University

Problem Specification
1. Create Geometry in GAMBITPre-Analysis & Start-up
2. Mesh Geometry in GAMBIT
3. Specify Boundary Types in GAMBITMesh
4. Set Up Problem in FLUENTSetup (Physics)
5. Solve!Solution
6. Analyze Results
7. Refine MeshVerification 7 Validation
Problem 1
Problem 2

Step 6:

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Results

Info
titleUseful Information

These instructions are for FLUENT 12. Click here for instructions for FLUENT 6.3.26.


Velocity Vector

Let's first look at the velocity vector in the nozzle.

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Code Block
(title "Static Pressure")

  (labels "Position" "Static Pressure")

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Code Block
((xy/key/label "centerline")

 

     \-0.5   5    97015.3

 

     \-0.48   48    96949.9


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.


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0.5    6012.92

 

)

 

   .   .   .   0.5    6012.92     )     ((xy/key/label "wall")

 

     \-0.5    100853

 

-0.480911    100496

 
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.

 
 

0.5    2874.7

 

5    100853     \-0.480911    100496    .   .   .       0.5    2874.7     )

Try copying the appropriate data sets to excel and plotting the results.

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Save this plot as machplot.xy by checking Write to File and clicking Write....

Go to Step 7: Refine MeshVerification & Validation

See and rate the complete Learning Module

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