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This special page shows all uploaded files.
| Date | Name | Thumbnail | Size | User | Description | Versions |
|---|---|---|---|---|---|---|
| 14:56, 20 November 2024 | Installed Engine scheme.svg (file) |  |
140 KB | Christian.Jente | 1 | |
| 14:43, 20 November 2024 | Installed Engine v2.pdf (file) |  |
75 KB | Christian.Jente | 1 | |
| 11:20, 20 November 2024 | Flapinserts nrt.png (file) |  |
1.88 MB | Christian.Jente | 1 | |
| 11:10, 20 November 2024 | Installed engine model2.png (file) |  |
139 KB | Christian.Jente | 1 | |
| 10:17, 20 November 2024 | Flap adjustment.png (file) |  |
443 KB | Christian.Jente | 1 | |
| 10:13, 20 November 2024 | Engine model at interface.png (file) |  |
136 KB | Christian.Jente | 1 | |
| 10:02, 20 November 2024 | Model vs facility axis in JExTRA.PNG (file) |  |
97 KB | Christian.Jente | 1 | |
| 09:24, 19 November 2024 | Near peak efficiency profile mesh.png (file) |  |
46 KB | Lionel.Temmerman | change of legend | 5 |
| 09:24, 19 November 2024 | Near peak temperature ratio mesh.png (file) |  |
46 KB | Lionel.Temmerman | change of legend | 4 |
| 09:23, 19 November 2024 | Near peak pressure ratio mesh.png (file) |  |
42 KB | Lionel.Temmerman | change of legend | 4 |
| 09:23, 19 November 2024 | Near peak angle profile mesh.png (file) |  |
34 KB | Lionel.Temmerman | change of legend | 4 |
| 09:22, 19 November 2024 | AC-6-16-near stall angle profile mesh.png (file) |  |
35 KB | Lionel.Temmerman | change of legend | 3 |
| 09:21, 19 November 2024 | AC6-16-near stall temperature ratio mesh.png (file) |  |
37 KB | Lionel.Temmerman | change of legend | 3 |
| 09:21, 19 November 2024 | AC-6-16-near stall efficiency profile mesh.png (file) |  |
38 KB | Lionel.Temmerman | change of legend | 3 |
| 09:21, 19 November 2024 | AC-6-16-near stall pressure ratio mesh.png (file) |  |
35 KB | Lionel.Temmerman | change of legend | 3 |
| 09:19, 19 November 2024 | AC6-16-eff vs pcqm sa fillet grid effect.png (file) |  |
43 KB | Lionel.Temmerman | change of legend | 3 |
| 09:18, 19 November 2024 | AC6-16-pr vs pcqm sa fillet grid effect.png (file) |  |
43 KB | Lionel.Temmerman | change of legend | 3 |
| 14:48, 8 November 2024 | AC6-16-surfacelines-ss-hub-sstlm.png (file) |  |
872 KB | Lionel.Temmerman | Surface lines on the hub and blade suction side for the lm sst model. | 1 |
| 14:46, 8 November 2024 | AC6-16-surfacelines-ss-hub-sst.png (file) |  |
899 KB | Lionel.Temmerman | Surface lines on the hub and blade suction side for the sst model. | 1 |
| 14:45, 8 November 2024 | AC6-16-surfacelines-hub-ss sstlm.png (file) |  |
682 KB | Lionel.Temmerman | Surface lines on the hub and blade pressure side for the lm-sst model. | 1 |
| 14:44, 8 November 2024 | AC6-16-surfacelines-hub-ss sst.png (file) |  |
717 KB | Lionel.Temmerman | Surface lines on the hub and blade pressure side for the sst model. | 1 |
| 15:38, 23 October 2024 | AC6-16-eff vs pcqm sa les.png (file) |  |
62 KB | Lionel.Temmerman | RANS renormalized | 4 |
| 15:37, 23 October 2024 | AC6-16-pr vs pcqm sa les.png (file) |  |
61 KB | Lionel.Temmerman | RANS renormalized | 6 |
| 14:07, 23 October 2024 | AC6-16-stall temperature ratio safran.png (file) |  |
36 KB | Lionel.Temmerman | AC6-16 - NASA Rotor 37 - SAFRAN - radial profile of total temperature ratio at stall. Revisited | 1 |
| 14:06, 23 October 2024 | AC6-16-stall pressure ratio safran.png (file) |  |
33 KB | Lionel.Temmerman | AC6-16 - NASA Rotor 37 - SAFRAN - radial profile of total pressure ratio at stall. Revisited | 1 |
| 14:06, 23 October 2024 | AC6-16-stall efficiency profile safran.png (file) |  |
35 KB | Lionel.Temmerman | AC6-16 - NASA Rotor 37 - SAFRAN - radial profile of efficiency at stall. Revisited | 1 |
| 12:32, 23 October 2024 | AC6-16-near peak temperature ratio safran.png (file) |  |
47 KB | Lionel.Temmerman | AC6-16 - NASA Rotor 37 - SAFRAN - radial profile of total temperature ratio at peak efficiency. Revisited. | 1 |
| 12:32, 23 October 2024 | AC6-16-near peak pressure ratio safran.png (file) |  |
42 KB | Lionel.Temmerman | AC6-16 - NASA Rotor 37 - SAFRAN - radial profile of total pressure ratio at peak efficiency. Revisited. | 1 |
| 12:31, 23 October 2024 | AC6-16-near peak efficiency profile safran.png (file) |  |
44 KB | Lionel.Temmerman | AC6-16 - NASA Rotor 37 - SAFRAN - radial profile of efficiency at peak efficiency. Revisited | 1 |
| 11:28, 23 October 2024 | AC6-16-pr vs pcqm safran turbulence.png (file) |  |
40 KB | Lionel.Temmerman | Total pressure ratio as a function of the normalized mass flow rate - effect of turbulence - SAFRAN | 1 |
| 11:27, 23 October 2024 | AC6-16-eff vs pcqm safran turbulence.png (file) |  |
39 KB | Lionel.Temmerman | Adiabatic efficiency as a function of the normalized mass flow rate - effect of turbulence - SAFRAN | 1 |
| 11:25, 23 October 2024 | AC6-16-eff vs pcqm sa.png (file) |  |
56 KB | Lionel.Temmerman | Change of normalisation | 2 |
| 11:24, 23 October 2024 | AC6-16-pr vs pcqm sa.png (file) |  |
62 KB | Lionel.Temmerman | Change of normalisation | 2 |
| 11:23, 23 October 2024 | AC6-16-pr vs pcqm 2eqs.png (file) |  |
61 KB | Lionel.Temmerman | Change of normalisation | 2 |
| 11:22, 23 October 2024 | AC6-16-eff vs pcqm 2eqs.png (file) |  |
52 KB | Lionel.Temmerman | Change of normalisation | 2 |
| 11:21, 23 October 2024 | AC6-16-pr vs pcqm earsm.png (file) |  |
60 KB | Lionel.Temmerman | Change of normalisation | 2 |
| 11:21, 23 October 2024 | AC6-16-eff vs pcqm earsm.png (file) |  |
56 KB | Lionel.Temmerman | Change of normalisation | 2 |
| 09:01, 23 October 2024 | AC6-16-pr vs pcqm safran scheme.png (file) |  |
41 KB | Lionel.Temmerman | Total pressure ratio as a function of a normalized flow rate (SAFRAN) - effect of numerical scheme. | 1 |
| 08:59, 23 October 2024 | AC6-16-eff vs pcqm safran scheme.png (file) |  |
41 KB | Lionel.Temmerman | Adiabatic efficiency as a function of the normalized mass flow rate (SAFRAN) - Effect of the scheme. | 1 |
| 08:58, 23 October 2024 | AC6-16-eff vs pcqm scheme.png (file) |  |
52 KB | Lionel.Temmerman | Update of normalization | 2 |
| 08:56, 23 October 2024 | AC6-16-pr vs pcqm scheme.png (file) |  |
55 KB | Lionel.Temmerman | Update of normalization | 2 |
| 14:00, 22 October 2024 | AC6-16-eff vs pcqm fillet rough.png (file) |  |
51 KB | Lionel.Temmerman | Change of normalization | 2 |
| 13:59, 22 October 2024 | AC6-16-pr vs pcqm fillet rough.png (file) |  |
54 KB | Lionel.Temmerman | Change of normalization | 2 |
| 13:30, 22 October 2024 | AC6-16-pr vs pcqm fillet transition.png (file) |  |
53 KB | Lionel.Temmerman | New normalization | 2 |
| 13:29, 22 October 2024 | AC6-16-eff vs pcqm fillet transition.png (file) |  |
49 KB | Lionel.Temmerman | New normalization | 2 |
| 12:25, 22 October 2024 | AC6-16-pr vs pcqm fillet shroud.png (file) |  |
50 KB | Lionel.Temmerman | change of normalization | 4 |
| 12:24, 22 October 2024 | AC6-16-eff vs pcqm fillet shroud.png (file) |  |
52 KB | Lionel.Temmerman | change of normalization | 6 |
| 11:46, 22 October 2024 | AC6-16-pr vs pcqm fillet nrbc.png (file) |  |
47 KB | Lionel.Temmerman | Effect of the treatment of the inlet and outlet bcs. Total pressure ratio as a function of the mass flow rate. | 1 |
| 11:45, 22 October 2024 | AC6-16-eff vs pcqm fillet nrbc.png (file) |  |
45 KB | Lionel.Temmerman | Effect of the treatment of the inlet and outlet bcs. Adiabatic efficiency as a function of the mass flow rate. | 1 |
| 11:28, 22 October 2024 | AC6-16-pr vs pcqm sa nofillet.png (file) |  |
43 KB | Lionel.Temmerman | change of normalization | 2 |
