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| Motion Pictures To see an animation, just click on one of the links below. To download a_hq.movie, click on the link with the right mouse button and choose the option "Save target as...". |
| Numerical simulation of hydrogen jet combustion in a supersonic air flow | |
989 Ko | |
| Flow calculation on a wind tunnel model configuration | |
452 Ko | |
| Wind tunnel test : jet pluming at the nozzle exit | |
948 Ko | |
| Result of a computation code : pressure field around the Marianne glider profile | |
259 Ko | |
| A glider subjected to flutter | |
548 Ko | |
| Aeroelastic computations on the Marianne glider wing structure | aleg2b_hq.mov |
222 Ko | |
| Spin testing on an ATL aircraft model in the vertical wind tunnel | aleg3_hq.mov |
1,25 Mo | |
| RCS of both stealthy and classical aircraft | |
972 Ko | |
| Simulation of "Cobra" and "HERBST" manoeuvres | |
1,28 Mo | |
| Wind tunnel testing of flight path | |
830 Ko | |
| Catapulting of an Airbus model through a smoke screen | |
1,30 Mo | |
| Flow visualisation on an A320 vertical stabiliser model | |
369 Ko | |
| Simulation of current distribution during a lightning strike on a Transall aircraft | |
239 Ko | |
| Ice accretion on a small scale airfoil in French Propulsion Test Center's (CEPr) Small Icing Loop (PAG) | |
884 Ko | |
| Film du contraste thermique relevé sur une plaque de carbone-époxy ayant reçu un impact. Mise en évidence d'un délaminage de plusieurs centimètres de long | |
1,23 Mo | |
| Simulation of the influence of the riveting process on the toughness of the assemblies | |
957 Ko | |
| Simulated dislocation movement | |
714 Ko | |
| Numerical simulation of the vortex flow | |
1,39 Mo | |
| Pressure measurement and triggering of the auto-ignition alert | |
8 Ko | |
| Wind tunnel testing of the AERAZUR D80 parafoil | |
918 Ko | |
| Blowdown visualisation on the model of a Soyuz capsule | |
884 Ko | |
| Ablation of a material during wind tunnel testing | |
734 Ko | |
| 2D unsteady Euler Computation | |
1,05 Mo | |
| Formation and development of vortices above an airfoil | |
188 Ko | |
| Direct Numerical Simulation of the flow near an optical cavity | |
1,07 Mo | |
| Flight computation on the Dauphin | |
1,16 Mo | |
| Calculated main rotor noise during descent | |
1,19 Mo | |
| Comparison of computed and measured results | |
589 Ko | |
| Numerical simulation by viscous-inviscid interaction | |
1,02 Mo | |
| Real-time testing at Mach 5 (approximately 5,500 km/h) : the darker regions correspond to the area of greatest heating | |
828 Ko | |
| Numerical simulation of the "Acoustic Resonance in Solid Propellant Motors" phenomenom | lanc2a_hq.mov |
365 Ko | |
| Consequences recorded during a firing test of acoustic resonance in solid propellant motors | lanc2b_hq.mov |
705 Ko | |
| Test of a miniaturised combustion chamber on the MASCOTTE facility | |
850 Ko | |
| Reflective regions on a missile impacted by a radar wave | |
778 Ko | |
| Flight testing of the Apache cruise missile (MATRA Defence source) | |
1,08 Mo | |
| Firing of the MPSR experimental missile and ground testing | |
1,85 Mo | |
| Principle of ramjet propulsion | miss3b_hq.mov |
1,36 Mo | |
| Computation of the combustion of drops in a ramjet | |
460 Ko | |
| 3D reproduction of an urban landscape by stereoscopy | |
684 Ko | |
| Agression scenario (VIGILE II data) | |
957 Ko | |
| Images de réflectance | opti1a_hq.mov |
450 Ko | |
| Images de distance | |
632 Ko | |
| Images without and with adaptative optics | |
356Ko | |
| Images of the MIR space station taken from 380 to 700 nautic miles away (raw images and registered images) | rad1a_hq.mov |
405 Ko | |
| Images of the MIR space station taken from 380 to 700 nautic miles away (raw images and registered images) | rad1b_hq.mov |
908 Ko | |
| A small utility car in motion along a runtrack : The Doppler effect makes it apparently taking a turn at 40mph across the fields ! | |
759 Ko | |
| Variations of the horizontal accuracy with time | |
1,65 Mo | |
| Columbia STS-7 flight "Life and Microgravity Science" (June 1996) | |
869 Ko | |
| Singular events and their consequences | |
1,06 Mo | |
| Liquid alloy atomized by argon gas jet | |
858 Ko | |
| Wake visualisation in a turbine stage (entropy) | |
432 Ko | |
| Elaboration of a TiAl ingot in a plasma furnace | |
1,26 Mo |
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