File list
From CFD-Wiki
This special page shows all uploaded files. By default the last uploaded files are shown at top of the list.
A click on a column header changes the sorting.| Date |  Name |
User | Size | Description | Versions |
|---|---|---|---|---|---|
| 22:37, 1 May 2006 | X-43A_(Hyper_-_X)_Mach_7_width_300px.jpg (file) | Jola | 16 KB | (NASA Dryden Flight Research Center ED97 43968-01 HYPER-X AT MACH 7: This CFD image is of the Hyper-X vehicle at the Mach 7 test condition with the engine operating.) | 1 |
| 17:41, 14 September 2007 | Wrinkled.jpg (file) | Joan | 29 KB | (Sketch of the wrinkled flamelet regime) | 1 |
| 15:32, 19 September 2005 | Wp_result.jpg (file) | Harish gopalan | 53 KB | 1 | |
| 09:21, 18 September 2012 | Wilson_4363.jpg (file) | GeneCardona4 | 140 KB | 1 | |
| 07:50, 19 September 2005 | Vtc_williams_main_cp.gif (file) | Praveen | 20 KB | (Pressure distribution on Williams airfoil) | 1 |
| 07:51, 19 September 2005 | Vtc_williams_flap_cp.gif (file) | Praveen | 23 KB | 1 | |
| 08:29, 19 September 2005 | Vtc_suddhoo_pressure_le.png (file) | Praveen | 24 KB | 1 | |
| 08:29, 19 September 2005 | Vtc_suddhoo_pressure.png (file) | Praveen | 21 KB | 1 | |
| 08:28, 19 September 2005 | Vtc_suddhoo_cp.png (file) | Praveen | 16 KB | 2 | |
| 08:23, 19 September 2005 | Vtc_suddhoo_airfoil.png (file) | Praveen | 7 KB | 1 | |
| 08:08, 19 September 2005 | Vtc_scramjet_geometry.png (file) | Praveen | 4 KB | 1 | |
| 07:52, 19 September 2005 | Vtc_scramjet_density.png (file) | Praveen | 10 KB | 1 | |
| 09:03, 16 September 2005 | Vtc_rae2822_pressure.png (file) | Praveen | 35 KB | (Pressure contours for RAE2822 airfoil at Mach=0.729, AOA=2.31 deg, Re=6.5 million) | 1 |
| 09:02, 16 September 2005 | Vtc_rae2822_mach.png (file) | Praveen | 33 KB | (Mach contours for RAE2822 airfoil at Mach=0.729, AOA=2.31 deg and Re=6.5 million) | 1 |
| 10:58, 16 September 2005 | Vtc_rae2822_grid.png (file) | Praveen | 21 KB | (Grid for RAE2822 airfoil) | 1 |
| 09:17, 16 September 2005 | Vtc_rae2822_cp.png (file) | Praveen | 14 KB | (Surface pressure coefficient for RAE2822 airfoil at Mach=0.729, AOA=2.31 deg and Re=6.5 million) | 1 |
| 23:54, 18 April 2008 | Vortex_vy.jpg (file) | Slffea | 10 KB | 3 | |
| 23:54, 18 April 2008 | Vortex_vx.jpg (file) | Slffea | 7 KB | 3 | |
| 22:22, 23 May 2007 | Vortex_streaklines.jpg (file) | Slffea | 71 KB | 1 | |
| 23:32, 18 April 2008 | Vortex_streaklines-15ang.jpg (file) | Slffea | 27 KB | 2 | |
| 23:55, 9 October 2007 | Vortex_streaklines-0ang2.jpg (file) | Slffea | 71 KB | (Streaklines for 0 angle of attack flow 16 seconds, 400 steps 102 x 45 grid dx = .266 dy = .266 dt = .04 ) | 1 |
| 23:29, 18 April 2008 | Vortex_streaklines-0ang.jpg (file) | Slffea | 29 KB | 3 | |
| 23:53, 18 April 2008 | Vortex_prs.jpg (file) | Slffea | 8 KB | 3 | |
| 23:35, 18 April 2008 | Vortex_pathlines-0ang.jpg (file) | Slffea | 31 KB | 1 | |
| 12:51, 16 October 2009 | Vofnaca0024results.jpg (file) | Jack1980 | 9 KB | 1 | |
| 12:46, 16 October 2009 | Vofnaca0024meshdetails.jpg (file) | Jack1980 | 30 KB | 2 | |
| 12:42, 16 October 2009 | Vofnaca0024experimentalsetup.jpg (file) | Jack1980 | 12 KB | 2 | |
| 12:18, 16 October 2009 | Vofnaca0024_results.JPG (file) | Jack1980 | 25 KB | 1 | |
| 12:17, 16 October 2009 | Vofnaca0024_experimental_setup.JPG (file) | Jack1980 | 32 KB | 1 | |
| 23:18, 4 October 2012 | Visit_steroidshq_2551.jpg (file) | AuroraLiu2 | 92 KB | 1 | |
| 09:34, 11 March 2016 | Validation.png (file) | Alisha | 26 KB | 2 | |
| 16:27, 15 September 2006 | VTC_circularcyl_geometry.png (file) | Jasond | 2 KB | (Typical circular cylinder domain) | 1 |
| 21:06, 1 September 2006 | VTC_JHflow_geometry.png (file) | Jasond | 5 KB | (Jeffery-Hamel flow geometry) | 2 |
| 21:00, 1 September 2006 | VTC_JHflow_3f.png (file) | Jasond | 21 KB | (Jeffery-Hamel flow similarity solution for 3 different constants) | 1 |
| 20:35, 15 September 2005 | V&tc_liddriven_ggsu.png (file) | Jasond | 6 KB | (Comparison of u/U at x/L=0.5: Fluent results and Ghia et al (1982)) | 1 |
| 20:33, 15 September 2005 | V&tc_liddriven_fluentu.png (file) | Jasond | 10 KB | (Contours of x-velocity (u) from Fluent) | 1 |
| 08:38, 16 September 2007 | Turbulence_Modeling_For_Beginners.pdf (file) | Tsaad | 193 KB | 1 | |
| 12:19, 11 May 2007 | Tioga_opacity_eos.jpg (file) | Xxdd | 294 KB | (Example of Tioga graphics.) | 1 |
| 10:09, 7 November 2007 | Time_corrolated_model.jpg (file) | Nejm | 17 KB | 1 | |
| 11:55, 7 November 2007 | Time_corrolated_model.JPG (file) | Nejm | 17 KB | 1 | |
| 12:05, 7 November 2007 | Time_corrolated_berlemont.JPG (file) | Nejm | 15 KB | 1 | |
| 09:02, 7 November 2007 | Time_corrolated.jpg (file) | Nejm | 16 KB | 1 | |
| 12:04, 7 November 2007 | Time_corrolated.JPG (file) | Nejm | 15 KB | 10 | |
| 15:17, 1 October 2007 | Time_correlated_model.jpg (file) | Nejm | 31 KB | 1 | |
| 16:39, 17 September 2007 | Thickened.jpg (file) | Joan | 45 KB | (Sketch of the thickened regime) | 1 |
| 10:54, 8 May 2007 | Thesis_RiteshKumar.pdf (file) | Riteshkd | 24 KB | ((The PhD thesis of Ritesh Kumar, Department of Mathematics, Indian Institute of Technology Kanpur. Submitted on Oct 2006. The work is devoted to the "Upwind based High Resolution Shock Capturing Schemes for Hyperbolic Conservation Laws") | 1 |
| 11:20, 29 January 2008 | Thermodynamicproperties.jpg (file) | Sega | 64 KB | (Critical cross-section and thermodynamic properties as a function of Mach-numer for stationary flow of an ideal gas containing two atoms (<math> \gamma = 1.4 </math>).) | 1 |
| 13:29, 22 May 2012 | Testupload.pdf (file) | Eanbbvbe | 79 KB | 1 | |
| 19:28, 16 September 2008 | StretchCompression.jpg (file) | Joan | 26 KB | (Reverted to version as of 19:26, 16 September 2008) | 5 |
| 13:23, 13 May 2011 | Stresses.JPG (file) | Michail | 21 KB | 2 |
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