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This special page shows all uploaded files.
| Date | Name | Thumbnail | Size | User | Description | Versions |
|---|---|---|---|---|---|---|
| 09:46, 14 May 2023 | CompContTravSys.png (file) |  |
83 KB | YannisTambom | 1 | |
| 09:46, 14 May 2023 | WindTunnel.png (file) |  |
51 KB | YannisTambom | 1 | |
| 13:00, 12 May 2023 | EXP dat LAT 90degrees.zip (file) |  |
36 KB | Stepan.Nosek | 1 | |
| 13:00, 12 May 2023 | EXP data LAT 45degrees.zip (file) | |
36 KB | Stepan.Nosek | 1 | |
| 08:58, 12 May 2023 | EXP data TOP 45degrees..zip (file) | |
55 KB | Stepan.Nosek | 1 | |
| 08:55, 12 May 2023 | EXP data TOP 90degrees.zip (file) | |
57 KB | Stepan.Nosek | 1 | |
| 12:09, 11 May 2023 | NetFLux 45.jpg (file) |  |
953 KB | Stepan.Nosek | 1 | |
| 12:01, 11 May 2023 | NetFLux 90.jpg (file) |  |
1,018 KB | Stepan.Nosek | 1 | |
| 11:05, 10 May 2023 | Measurement Technique LDAadnFFID.jpg (file) |  |
915 KB | Stepan.Nosek | 2 | |
| 20:08, 9 May 2023 | BL Profiles positions.jpg (file) |  |
391 KB | Stepan.Nosek | 1 | |
| 14:25, 9 May 2023 | 3D Tunel Num.jpg (file) |  |
392 KB | Stepan.Nosek | 1 | |
| 11:52, 9 May 2023 | Ur crossflow.png (file) |  |
28 KB | YannisTambom | 1 | |
| 11:02, 9 May 2023 | Windward liquid sheet.png (file) |  |
130 KB | YannisTambom | 1 | |
| 10:17, 9 May 2023 | Droplet size spectra.png (file) |  |
37 KB | YannisTambom | Fig 2b EXP1 (Intro) | 1 |
| 08:38, 9 May 2023 | Opti meas wt section.png (file) |  |
357 KB | YannisTambom | Fig 1b from EXP1 (Abstract) | 1 |
| 08:37, 9 May 2023 | Spray image hs im.png (file) |  |
246 KB | YannisTambom | Fig 1 from EXP1 (Abstract) | 1 |
| 11:58, 3 May 2023 | GraphAbstract EXP1-2.jpg (file) |  |
621 KB | Stepan.Nosek | 1 | |
| 11:49, 3 May 2023 | Graphical abstract EXP1-2.jpg (file) |  |
621 KB | Stepan.Nosek | 1 | |
| 10:06, 3 April 2023 | AC6-16-figure 20.png (file) |  |
57 KB | Lionel.Temmerman | 2 | |
| 09:48, 3 April 2023 | AC6-16-figure 29-maxflow.png (file) |  |
21 KB | Lionel.Temmerman | Contours of the relative Mach number in a blade-to-balde view along the 95% streamsurface for design at max flow condition. The dash line indicates the trajectory of the tip leakage vortex. (Taken from figure 29 in Suder (1996)). | 1 |
| 09:47, 3 April 2023 | AC6-16-figure 29-highflow.png (file) |  |
20 KB | Lionel.Temmerman | Contours of the relative Mach number in a blade-to-balde view along the 95% streamsurface for design at high flow condition. The dash line indicates the trajectory of the tip leakage vortex. (Taken from figure 29 in Suder (1996)). | 1 |
| 09:46, 3 April 2023 | AC6-16-figure 29-lowflow.png (file) |  |
17 KB | Lionel.Temmerman | Contours of the relative Mach number in a blade-to-balde view along the 95% streamsurface for design at low flow condition. The dash line indicates the trajectory of the tip leakage vortex. (Taken from figure 29 in Suder (1996)). | 1 |
| 09:31, 3 April 2023 | AC-16-figure 23-maxflow.png (file) |  |
20 KB | Lionel.Temmerman | Contours of the relative Mach number number in a blade-to-blade view along the 70% streamsurface for design speed and max flow condition. (Taken from figure 23 in Suder (1996)) | 1 |
| 09:20, 3 April 2023 | AC-16-figure 23-highflow.png (file) |  |
18 KB | Lionel.Temmerman | Contours of the relative Mach number number in a blade-to-blade view along the 70% streamsurface for design speed and high flow condition. (Taken from figure 23 in Suder (1996)) | 1 |
| 09:59, 30 March 2023 | AC6-16-TRZ4 92.csv (file) | |
610 bytes | Lionel.Temmerman | Total temperature ratio at station 4 for 92 % of the mass flow rate at design speed. | 1 |
| 09:58, 30 March 2023 | AC6-16-TRZ4 98.csv (file) | |
610 bytes | Lionel.Temmerman | Total temperature ratio at station 4 for 98 % of the mass flow rate at design speed. | 1 |
| 09:58, 30 March 2023 | AC6-16-TRZ3 98.csv (file) | |
661 bytes | Lionel.Temmerman | Total temperature ratio at station 3 for 98 % of the mass flow rate at design speed. | 1 |
| 09:57, 30 March 2023 | AC6-16-TRZ3 92.csv (file) | |
695 bytes | Lionel.Temmerman | Total temperature ratio at station 3 for 92 % of the mass flow rate at design speed. | 1 |
| 09:57, 30 March 2023 | AC6-16-TANZ4 98.csv (file) | |
677 bytes | Lionel.Temmerman | Tangential velocity normalized by the tip speed at station 4 for 98 % of the mass flow rate at design speed. | 1 |
| 09:56, 30 March 2023 | AC6-16-TANZ4 92.csv (file) | |
677 bytes | Lionel.Temmerman | Tangential velocity normalized by the tip speed at station 4 for 92 % of the mass flow rate at design speed. | 1 |
| 09:56, 30 March 2023 | AC6-16-TANZ3 98.csv (file) | |
731 bytes | Lionel.Temmerman | Tangential velocity normalized by the tip speed at station 3 for 98 % of the mass flow rate at design speed. | 1 |
| 09:55, 30 March 2023 | AC6-16-TANZ3 92.csv (file) | |
767 bytes | Lionel.Temmerman | Tangential velocity normalized by the tip speed at station 3 for 92 % of the mass flow rate at design speed. | 1 |
| 09:52, 30 March 2023 | AC6-16-PRZ4 98.csv (file) | |
604 bytes | Lionel.Temmerman | Total pressure ratio at station 4 for 98 % of the mass flow rate at design speed. | 1 |
| 09:51, 30 March 2023 | AC6-16-PRZ4 92.csv (file) | |
604 bytes | Lionel.Temmerman | Total pressure ratio at station 4 for 92 % of the mass flow rate at design speed. | 1 |
| 09:50, 30 March 2023 | AC6-16-PR ALL.csv (file) | |
440 bytes | Lionel.Temmerman | Pressure ratio as a function of the mass flow rate at design speed. | 1 |
| 09:47, 30 March 2023 | AC6-16-EFFZ4 98.csv (file) | |
623 bytes | Lionel.Temmerman | Adiabatic efficiency at station 4 for 98 % of the mass flow rate at design speed. | 1 |
| 09:46, 30 March 2023 | AC6-16-EFFZ4 92.csv (file) | |
623 bytes | Lionel.Temmerman | Adiabatic efficiency at station 4 for 92 % of the mass flow rate at design speed. | 1 |
| 09:44, 30 March 2023 | AC6-16-EFF ALL.csv (file) | |
454 bytes | Lionel.Temmerman | adiabatic efficiency as a function of the mass flow rate at design speed. | 1 |
| 09:43, 30 March 2023 | AC6-16-ANGZ4 98.csv (file) | |
603 bytes | Lionel.Temmerman | Absolute flow angle at station 4 for 98 % of the mass flow rate at design speed. | 1 |
| 09:17, 30 March 2023 | AC6-16-ANGZ4 92.csv (file) | |
603 bytes | Lionel.Temmerman | Absolute flow angle at station 4 for 92 % of the mass flow rate at design speed. | 1 |
| 09:17, 30 March 2023 | AC6-16-ANGZ3 98.csv (file) | |
654 bytes | Lionel.Temmerman | Absolute flow angle at station 3 for 98 % of the mass flow rate at design speed. | 1 |
| 08:29, 30 March 2023 | AC6-16-ANGZ3 92.csv (file) | |
688 bytes | Lionel.Temmerman | Absolute flow angle at station 3 for 92 % of the mass flow rate at design speed. | 1 |
| 12:52, 15 March 2023 | Inlet profile.csv (file) | |
636 bytes | Lionel.Temmerman | AC6-16: inlet profile for NASA rotor 37 (#station 1) | 1 |
| 14:52, 14 March 2023 | EXP Template.pdf (file) |  |
511 KB | Mike | 2 | |
| 10:24, 7 March 2023 | AC6-16 geometry rotor 37.geomTurbo (file) | |
180 KB | Lionel.Temmerman | Geometry file for NASA rotor 37 (geomTurbo format). | 1 |
| 23:25, 26 February 2023 | DNS1-6 Wing-body junction bottom streamlines.png (file) |  |
915 KB | Alessandro.colombo | 3 | |
| 16:52, 24 February 2023 | DNS1-6 Wing-body junction midplane averaged velocity x.png (file) |  |
145 KB | Alessandro.colombo | 4 | |
| 16:51, 24 February 2023 | DNS1-6 Wing-body junction midplane averaged velocity y.png (file) |  |
148 KB | Alessandro.colombo | 3 | |
| 16:45, 24 February 2023 | DNS1-6 Wing-body junction midplane TKE.png (file) |  |
149 KB | Alessandro.colombo | 3 | |
| 16:42, 24 February 2023 | DNS1-6 Wing-body junction midplane Reynolds stress zz.png (file) |  |
170 KB | Alessandro.colombo | 3 |
