User contributions for Lionel.Temmerman
Jump to navigation
Jump to search
16 April 2024
- 07:5607:56, 16 April 2024 diff hist 0 File:AC-6-16 pr vs span exp near stall.png Lionel.Temmerman uploaded a new version of File:AC-6-16 pr vs span exp near stall.png current
- 07:5507:55, 16 April 2024 diff hist 0 File:AC-6-16 eff vs span exp peak.png Lionel.Temmerman uploaded a new version of File:AC-6-16 eff vs span exp peak.png
- 07:5407:54, 16 April 2024 diff hist 0 File:AC-6-16 eff vs span exp near stall.png Lionel.Temmerman uploaded a new version of File:AC-6-16 eff vs span exp near stall.png current
- 07:5307:53, 16 April 2024 diff hist 0 File:AC-6-16 ang vs span exp peak.png Lionel.Temmerman uploaded a new version of File:AC-6-16 ang vs span exp peak.png
- 07:3007:30, 16 April 2024 diff hist 0 File:AC-6-16 ang vs span exp near stall.png Lionel.Temmerman uploaded a new version of File:AC-6-16 ang vs span exp near stall.png current
- 07:2707:27, 16 April 2024 diff hist 0 File:AC-6-16 eff vs qm exp.png Lionel.Temmerman uploaded a new version of File:AC-6-16 eff vs qm exp.png current
5 April 2024
- 16:2616:26, 5 April 2024 diff hist −2,937 Lib:Test Data AC6-16 No edit summary
- 16:2516:25, 5 April 2024 diff hist −44 Lib:Test Data AC6-16 No edit summary
- 16:2416:24, 5 April 2024 diff hist +805 Lib:Test Data AC6-16 No edit summary
- 16:1616:16, 5 April 2024 diff hist 0 Lib:Test Data AC6-16 No edit summary
- 16:1516:15, 5 April 2024 diff hist +38 Lib:Test Data AC6-16 No edit summary
- 16:1116:11, 5 April 2024 diff hist +329 Lib:Test Data AC6-16 No edit summary
- 16:0416:04, 5 April 2024 diff hist +52 Lib:Test Data AC6-16 No edit summary
- 15:5815:58, 5 April 2024 diff hist +116 N File:AC-6-16 tr vs qm exp.png Total temperature ratio as a function of the mass flow rate - experimental data for the NASA rotor 37. current
- 15:5815:58, 5 April 2024 diff hist +113 N File:AC-6-16 pr vs qm exp.png Total pressure ratio as a function of the mass flow rate - experimental data for the NASA rotor 37. current
- 15:5715:57, 5 April 2024 diff hist +113 N File:AC-6-16 eff vs qm exp.png Adiabatic Efficiency as a function of the mass flow rate - experimental data for the NASA rotor 37.
- 15:5615:56, 5 April 2024 diff hist +139 N File:AC-6-16 tr vs span exp peak.png Total temperature ratio as a function of the span (%) at peak efficiency condition - experimental data for the NASA rotor 37.
- 15:5515:55, 5 April 2024 diff hist +134 N File:AC-6-16 tr vs span exp near stall.png Total temperature ratio as a function of the span (%) at near-stall condition - experimental data for the NASA rotor 37.
- 15:5515:55, 5 April 2024 diff hist +136 N File:AC-6-16 pr vs span exp peak.png Total pressure ratio as a function of the span (%) at peak efficiency condition - experimental data for the NASA rotor 37.
- 15:5415:54, 5 April 2024 diff hist +131 N File:AC-6-16 pr vs span exp near stall.png Total pressure ratio as a function of the span (%) at near-stall condition - experimental data for the NASA rotor 37.
- 15:5315:53, 5 April 2024 diff hist +136 N File:AC-6-16 eff vs span exp peak.png Adiabatic efficiency as a function of the span (%) at peak efficiency condition - experimental data for the NASA rotor 37.
- 15:5315:53, 5 April 2024 diff hist +131 N File:AC-6-16 eff vs span exp near stall.png Adiabatic efficiency as a function of the span (%) at near-stall condition - experimental data for the NASA rotor 37.
- 15:5115:51, 5 April 2024 diff hist +131 N File:AC-6-16 ang vs span exp peak.png Flow angle (°) as a function of the span (%) at peak efficiency condition - experimental data for the NASA rotor 37.
- 15:5115:51, 5 April 2024 diff hist +126 N File:AC-6-16 ang vs span exp near stall.png Flow angle (°) as a function of the span (%) at near-stall condition - experimental data for the NASA rotor 37.
4 April 2024
- 13:1513:15, 4 April 2024 diff hist +1,819 Lib:Test Data AC6-16 →Measured Data
- 12:4012:40, 4 April 2024 diff hist −5 Lib:Test Data AC6-16 →Boundary Data
3 April 2024
- 15:0515:05, 3 April 2024 diff hist −3,805 Lib:Test Data AC6-16 →Overview of Tests
4 April 2023
- 08:4308:43, 4 April 2023 diff hist −16 Lib:Test Data AC6-16 →Overview of Tests
- 08:4208:42, 4 April 2023 diff hist +219 Lib:Test Data AC6-16 →Overview of Tests
- 08:2508:25, 4 April 2023 diff hist +1,027 Lib:Test Data AC6-16 →TEST CASE EXP3 - 60 % of the design speed
- 08:2308:23, 4 April 2023 diff hist +633 Lib:Test Data AC6-16 →Measured Data
- 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