Uploads by Lionel.Temmerman
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This special page shows all uploaded files.
| Date | Name | Thumbnail | Size | Description | Versions |
|---|---|---|---|---|---|
| 09:43, 16 April 2024 | AC6-16 min RANS bound temperatureratio vs span AGARD.csv (file) |  |
1 KB | Lower RANS bound from AGARD for total temperature ratio as a function of the span location (digitized). | 1 |
| 09:42, 16 April 2024 | AC6-16 max RANS bound temperatureratio vs span AGARD.csv (file) | |
2 KB | Upper RANS bound from AGARD for total temperature ratio as a function of the span location (digitized). | 1 |
| 09:42, 16 April 2024 | AC6-16 min RANS bound pressureratio vs span AGARD.csv (file) | |
1 KB | Lower RANS bound from AGARD for total pressure ratio as a function of the span location (digitized). | 1 |
| 09:41, 16 April 2024 | AC6-16 max RANS bound pressureratio vs span AGARD.csv (file) | |
2 KB | Upper RANS bound from AGARD for total pressure ratio as a function of the span location (digitized). | 1 |
| 09:41, 16 April 2024 | AC6-16 min RANS bound eff vs span AGARD.csv (file) | |
1 KB | Lower RANS bound from AGARD for efficiency as a function of the span location (digitized). | 1 |
| 09:40, 16 April 2024 | AC6-16 max RANS bound eff vs span AGARD.csv (file) | |
2 KB | Upper RANS bound from AGARD for efficiency as a function of the span location (digitized). | 1 |
| 09:40, 16 April 2024 | AC6-16 min RANS bound pressureratio vs qn AGARD.csv (file) | |
395 bytes | Lower RANS bound from AGARD for total pressure ratio as a function of the normalized mass flow rate (digitized). | 1 |
| 09:39, 16 April 2024 | AC6-16 max RANS bound pressureratio vs qn AGARD.csv (file) | |
323 bytes | Upper RANS bound from AGARD for total pressure ratio as a function of the normalized mass flow rate (digitized). | 1 |
| 09:38, 16 April 2024 | AC6-16 min RANS bound eff vs qn AGARD.csv (file) | |
354 bytes | Lower RANS bound from AGARD for efficiency as a function of the normalized mass flow rate (digitized). | 1 |
| 09:38, 16 April 2024 | AC6-16 max RANS bound eff vs qn AGARD.csv (file) | |
339 bytes | Upper RANS bound from AGARD for efficiency as a function of the normalized mass flow rate (digitized). | 1 |
| 07:58, 16 April 2024 | AC-6-16 tr vs span exp peak.png (file) |  |
26 KB | 2 | |
| 07:57, 16 April 2024 | AC-6-16 tr vs span exp near stall.png (file) |  |
25 KB | 2 | |
| 07:57, 16 April 2024 | AC-6-16 pr vs span exp peak.png (file) |  |
26 KB | 2 | |
| 07:56, 16 April 2024 | AC-6-16 pr vs span exp near stall.png (file) |  |
25 KB | 2 | |
| 07:55, 16 April 2024 | AC-6-16 eff vs span exp peak.png (file) |  |
26 KB | 2 | |
| 07:54, 16 April 2024 | AC-6-16 eff vs span exp near stall.png (file) |  |
25 KB | 2 | |
| 07:53, 16 April 2024 | AC-6-16 ang vs span exp peak.png (file) |  |
24 KB | 2 | |
| 07:30, 16 April 2024 | AC-6-16 ang vs span exp near stall.png (file) |  |
23 KB | 2 | |
| 07:27, 16 April 2024 | AC-6-16 eff vs qm exp.png (file) |  |
26 KB | 2 | |
| 15:58, 5 April 2024 | AC-6-16 tr vs qm exp.png (file) |  |
24 KB | Total temperature ratio as a function of the mass flow rate - experimental data for the NASA rotor 37. | 1 |
| 15:58, 5 April 2024 | AC-6-16 pr vs qm exp.png (file) |  |
24 KB | Total pressure ratio as a function of the mass flow rate - experimental data for the NASA rotor 37. | 1 |
| 10:06, 3 April 2023 | AC6-16-figure 20.png (file) |  |
57 KB | 2 | |
| 09:48, 3 April 2023 | AC6-16-figure 29-maxflow.png (file) |  |
21 KB | 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 | 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 | 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 | 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 | 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 | 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 | 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 | 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 | 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 | 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 | 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 | 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 | 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 | 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 | 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 | 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 | 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 | 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 | 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 | 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 | 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 | 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 | 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 | AC6-16: inlet profile for NASA rotor 37 (#station 1) | 1 |
| 10:24, 7 March 2023 | AC6-16 geometry rotor 37.geomTurbo (file) | |
180 KB | Geometry file for NASA rotor 37 (geomTurbo format). | 1 |
| 16:44, 23 February 2023 | Test facility.png (file) |  |
56 KB | General view of the test facility (taken from the Agard report) | 1 |
| 16:44, 23 February 2023 | Measurements-stations.png (file) |  |
44 KB | View of the different measurement locations in the axial direction. | 1 |
| 16:43, 23 February 2023 | Cut view of the blade.png (file) |  |
22 KB | Cross-sectional view of the blade (taken from the AGARD report). | 1 |
