Uploads by LESQWALL
Jump to navigation
Jump to search
This special page shows all uploaded files.
| Date | Name | Thumbnail | Size | Description | Versions |
|---|---|---|---|---|---|
| 16:13, 5 April 2013 | UFR4-15 VelocityPJICF.jpg (file) |  |
191 KB | 1 | |
| 16:06, 5 April 2013 | UFR4-15 Procedure.jpg (file) |  |
58 KB | 1 | |
| 15:45, 5 April 2013 | UFR4-15 DieselJet.jpg (file) |  |
46 KB | 1 | |
| 15:44, 5 April 2013 | UFR4-15 Convergent2.jpg (file) |  |
90 KB | 1 | |
| 15:38, 5 April 2013 | UFR4-15 CFlow.jpg (file) |  |
126 KB | 1 | |
| 15:26, 5 April 2013 | UFR4-15 VProfileI.jpg (file) |  |
186 KB | 1 | |
| 15:26, 5 April 2013 | UFR4-15 FRateII.jpg (file) |  |
171 KB | 1 | |
| 14:58, 5 April 2013 | UFR4-15 HResonator.jpg (file) |  |
73 KB | 1 | |
| 14:58, 5 April 2013 | UFR4-15 FRateI.jpg (file) |  |
45 KB | 1 | |
| 14:38, 5 April 2013 | UFR4-15 Mesh.jpg (file) |  |
107 KB | 1 | |
| 14:37, 5 April 2013 | UFR4-15 Geometry.jpg (file) |  |
16 KB | 1 | |
| 13:16, 5 April 2013 | UFR4-15 Convergent.jpg (file) |  |
90 KB | 2 | |
| 12:55, 5 April 2013 | UFR 15 Diesel Jet.jpg (file) |  |
46 KB | Schematic diagram depicting the conceptual model of diesel jet combustion in the jet impinging wall configuration (LIF stands for Laser Induced Fluorescence). | 1 |
| 07:26, 20 June 2012 | UFR4-15 P2-Velocity.jpg (file) |  |
123 KB | Influence of the SGS viscosity model on the velocity field in plane P2 at (a) t = 1.8 (b) t = 2.0 ms (c) t = 3.0 ms | 1 |
| 07:26, 20 June 2012 | UFR4-15 P5-Velocity-2.jpg (file) |  |
138 KB | Influence of the SGS viscosity model on the velocity field in plane P5 at (a) t = 4.0 (b) t = 5.0 ms (c) t = 6.0 ms | 1 |
| 07:25, 20 June 2012 | UFR4-15 P5-Velocity.jpg (file) |  |
292 KB | Influence of the SGS viscosity model on the Velocity field in plane P5 at (a) t = 0.8 (b) t = 1.2 ms (c) t = 1.6 ms (d) t = 1.8 ms (e) t = 2.0 ms (f) t = 3.0 ms | 1 |
| 16:16, 19 June 2012 | UFR4-15 H-Convergent.jpg (file) |  |
62 KB | Schematic description of an Helmholtz resonator as described in [29]. | 1 |
| 16:15, 19 June 2012 | UFR4-15 Flow-rate.jpg (file) |  |
57 KB | Flow rate of the injector without cross flow and without impinging surface. | 1 |
| 16:15, 19 June 2012 | UFR4-15 PIV-T1000.jpg (file) |  |
152 KB | Velocity vector field of the jet at t = 1.0 ms (without impinging surface) | 1 |
| 15:48, 19 June 2012 | UFR4-15 PIV-Set-up.jpg (file) |  |
22 KB | Schematic description of the PIV set-up for a given plane: M stands for mirror, SL the spherical lens and CL the cylindrical lens | 1 |
| 15:37, 19 June 2012 | UFR4-15 PIV-Planes.jpg (file) |  |
86 KB | Lateral and top view of the PIV planes (dimensions shown in mm). | 1 |
| 14:38, 19 June 2012 | UFR4-15 Lab.jpg (file) |  |
238 KB | Experimental apparatus with the PIV set-up | 1 |
| 14:37, 19 June 2012 | UFR4-15 PJICF.jpg (file) |  |
122 KB | Schematic description of the experimental set-up of the hot impinging pulsed jet in presence of a cross flow. | 1 |
| 16:45, 15 June 2012 | Theory PJICF.png (file) |  |
157 KB | FIG. 1: Flow features of the PJICF: (1) Vortex roll-up and propagation, (2) stagnation region, (3)shear and boundary layers, (4) wall heat transfer (but not discussed here) | 1 |
