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Main Web>Go4HybridTestCases>TestCase007RoundJetAeroacoustics (2015-10-16, AlistairRevell)
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Main Web>Go4HybridTestCases>TestCase007RoundJetAeroacoustics (2015-10-16, AlistairRevell)
Round Jet Aeroacousticsback to test case home | |
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Coordinator: CFDB Data Originator: Data Type: Numerical Case Status: 
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Page Contents |
Description
- TCI5_M01_jetProposalCFDB.pptx: Slides from first meeting
- I5_TC_definition_draft_v4.docx: test case description document
Flow Parameters
Boundary conditions:- SA_profiles.dat: Nozzle exit profiles from precursor SA-RANS of nozzle interior (provided by NTS)
Meshes
Meshes available for this case are listed in the table. Meshes marked with M are mandatory.
| Mesh Description | File | Coordinator | Number of cells | Mesh Format | Mesh Generator |
|---|---|---|---|---|---|
| G1 (Fluent) |  |
N/A | 1.5 million | other | (not set) |
| G2 (Fluent) | |
N/A | 4.3 million | other | (not set) |
| G3 (Fluent) M | |
N/A | 8.8 million | other | (not set) |
| G1 (Tecplot) | |
N/A | 1.5 million | tecplot | (not set) |
| G2 (Tecplot) | |
N/A | 4.3 million | tecplot | (not set) |
| G3 (Tecplot) M | |
N/A | 8.8 million | tecplot | (not set) |
Results
Simulation results available for this case are listed below.
| I | Attachment | Action | Size | Date | Who | Comment |
|---|---|---|---|---|---|---|
 docx |
I5_TC_definition_draft_v4.docx | manage | 439.6 K | 2014-10-21 - 14:25 | UnknownUser | |
| dat |
SA_profiles.dat | manage | 457.5 K | 2014-09-25 - 14:20 | UnknownUser | |
| pptx |
TCI5_M01_jetProposalCFDB.pptx | manage | 4182.3 K | 2014-01-01 - 16:46 | AlistairRevell |
Topic revision: r8 - 2015-10-16 - 18:49:11 - AlistairRevell
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