User contributions for Lionel.Temmerman
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4 April 2023
- 08:2208:22, 4 April 2023 diff hist 0 Lib:Test Data AC6-16 →Measured Data
- 08:2108:21, 4 April 2023 diff hist +223 Lib:Test Data AC6-16 →Measured Data
- 08:1908:19, 4 April 2023 diff hist +154 Lib:Test Data AC6-16 →TEST CASE EXP2 - 80 % of the design speed
- 06:3406:34, 4 April 2023 diff hist +856 Lib:Test Data AC6-16 →TEST CASE EXP3 - 60 % of the design speed
- 06:3306:33, 4 April 2023 diff hist +855 Lib:Test Data AC6-16 →TEST CASE EXP2 - 80 % of the design speed
- 06:3206:32, 4 April 2023 diff hist +168 Lib:Test Data AC6-16 →Boundary Data
3 April 2023
- 10:0710:07, 3 April 2023 diff hist +911 Lib:Test Data AC6-16 →Measured Data
- 10:0610:06, 3 April 2023 diff hist 0 File:AC6-16-figure 20.png Lionel.Temmerman uploaded a new version of File:AC6-16-figure 20.png
- 09:4809:48, 3 April 2023 diff hist +243 N File:AC6-16-figure 29-maxflow.png 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)).
- 09:4709:47, 3 April 2023 diff hist +244 N File:AC6-16-figure 29-highflow.png 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)).
- 09:4609:46, 3 April 2023 diff hist +243 N File:AC6-16-figure 29-lowflow.png 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)).
- 09:3109:31, 3 April 2023 diff hist +190 N File:AC-16-figure 23-maxflow.png 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))
- 09:2009:20, 3 April 2023 diff hist +191 N File:AC-16-figure 23-highflow.png 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))
- 09:0909:09, 3 April 2023 diff hist +152 N File:AC6-16-figure 20.png Contours of relative Mach number along the 70% streamsurface for the rotor operating at design speed and low flow condition. (Suder, 1996)
30 March 2023
- 16:1016:10, 30 March 2023 diff hist 0 Lib:Description AC6-16 →The NASA Rotor-37
- 16:1016:10, 30 March 2023 diff hist 0 Lib:CFD Simulations AC6-16 →References
- 16:0916:09, 30 March 2023 diff hist 0 Lib:Best Practice Advice AC6-16 →Recommendations for Future Work
- 16:0816:08, 30 March 2023 diff hist 0 Lib:Evaluation AC6-16 →Comparison of Test Data and CFD
- 16:0616:06, 30 March 2023 diff hist +88 Lib:CFD Simulations AC6-16 →CFD Results
- 16:0516:05, 30 March 2023 diff hist +491 Lib:CFD Simulations AC6-16 →Application of Physical Models
- 15:5715:57, 30 March 2023 diff hist +368 Lib:CFD Simulations AC6-16 →Numerical Accuracy
- 15:5115:51, 30 March 2023 diff hist +5 Lib:CFD Simulations AC6-16 →Computational Domain
- 15:5015:50, 30 March 2023 diff hist +1,107 Lib:CFD Simulations AC6-16 →Solution Strategy
- 15:3515:35, 30 March 2023 diff hist +6 Lib:CFD Simulations AC6-16 →Computational Domain
- 15:3415:34, 30 March 2023 diff hist +66 Lib:CFD Simulations AC6-16 →Computational Domain
- 15:3315:33, 30 March 2023 diff hist +1,081 Lib:CFD Simulations AC6-16 →Boundary Conditions
- 15:1415:14, 30 March 2023 diff hist −20 Lib:CFD Simulations AC6-16 →Computational Domain
- 15:1015:10, 30 March 2023 diff hist +3 Lib:CFD Simulations AC6-16 →Overview of CFD Simulations
- 15:0615:06, 30 March 2023 diff hist +2,218 Lib:CFD Simulations AC6-16 →Overview of CFD Simulations
- 14:3414:34, 30 March 2023 diff hist +67 Lib:Test Data AC6-16 →TEST CASE EXP1 - 100 % of the design speed
- 14:0714:07, 30 March 2023 diff hist +305 Lib:CFD Simulations AC6-16 →Overview of CFD Simulations
- 14:0514:05, 30 March 2023 diff hist −1 Lib:CFD Simulations AC6-16 →SIMULATION CASE CFD2
- 14:0514:05, 30 March 2023 diff hist −2 Lib:CFD Simulations AC6-16 →SIMULATION CASE CFD1
- 13:5313:53, 30 March 2023 diff hist +88 Lib:Test Data AC6-16 →Overview of Tests
- 13:4613:46, 30 March 2023 diff hist +50 Lib:Test Data AC6-16 →Overview of Tests
- 13:4613:46, 30 March 2023 diff hist −24 Lib:Test Data AC6-16 →TEST CASE EXP1
- 13:4113:41, 30 March 2023 diff hist +351 Lib:Test Data AC6-16 →Measured Data
- 12:5312:53, 30 March 2023 diff hist +232 Lib:Test Data AC6-16 →Measured Data
- 12:0712:07, 30 March 2023 diff hist +117 Lib:AC6-16 →Abstract
- 11:5611:56, 30 March 2023 diff hist +914 Lib:Test Data AC6-16 →Measured Data
- 11:3011:30, 30 March 2023 diff hist +6 Lib:Best Practice Advice AC6-16 →Best Practice Advice
- 11:2911:29, 30 March 2023 diff hist +6 Lib:Evaluation AC6-16 →Comparison of Test Data and CFD
- 11:2811:28, 30 March 2023 diff hist +6 Lib:CFD Simulations AC6-16 →Overview of CFD Simulations
- 11:2711:27, 30 March 2023 diff hist +6 Lib:Test Data AC6-16 →References
- 11:2611:26, 30 March 2023 diff hist +6 Lib:Description AC6-16 →The NASA Rotor-37
- 11:2611:26, 30 March 2023 diff hist 0 Lib:AC6-16 →Abstract
- 11:1811:18, 30 March 2023 diff hist +4 Lib:AC6-16 →Abstract
- 11:1711:17, 30 March 2023 diff hist +2 Lib:AC6-16 →Abstract
- 09:5909:59, 30 March 2023 diff hist +98 N File:AC6-16-TRZ4 92.csv Total temperature ratio at station 4 for 92 % of the mass flow rate at design speed. current
- 09:5809:58, 30 March 2023 diff hist +98 N File:AC6-16-TRZ4 98.csv Total temperature ratio at station 4 for 98 % of the mass flow rate at design speed. current