| 1. | Propulsion aérobie et autres systèmes énergétiques - moyens d'essais - Offre technologique Onera |
| | AdvantagesUnique testing facilities in Europe : auto-ignition combustion testing and High Pressure High Temperature testing (1000 K, 40 bar, 4kg / s) : powerful, flexible testing facilities, exceptionally close to industrial applications.. Simulation and development of supersonic combustion chambers.. |
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| 2. | Modélisation numérique et exploration expérimentale des écoulements réactifs multiphasiques pour des moteurs aéronautiques et spatiaux - Offre technologique Onera |
| | New LACOM facility for experimental investigation of two-phase flow phenomena in high pressure and temperature environment (P = 1 - 50 bar, T = 300 - 1000 K, air mass flow-rate = 0.1 - 1 kg / s)... |
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| 3. | Air-Breathing Propulsion and Other Energetic Systems : Testing Facilities - Onera's Technological Offer |
| | Unique testing facilities in Europe : auto-ignition combustion testing and High Pressure High Temperature testing (1000 K, 40 bar, 4kg / s) : powerful, flexible testing facilities, exceptionally close to industrial applications.... High Pressure High Temperature (HPHT), (1000K, 40 bar, 4kg / s) combustion testing.... |
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| 4. | Mascotte, a cryogenic combustion research test bench - ONERA / DEFA-EN |
| | High pressure combustor... |
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| 5. | A Cryogenic Combustion Research Test Bench, LOX / Methane Configuration - ONERA / DEFA-EN |
| | Since its first version, V01 (oxygen / hydrogen at low pressure), the bench has undergone a number of changes to its latest version, V04 (oxygen / methane at high pressure).... |
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| 6. | Main Propulsion Test Stands (ATD - LAERTE) - ONERA / DEFA-EN |
| | High-pressure air compressors... Essentially, these facilities include a three-stage compressor delivering a continuous air flow of 10 kg / s at 12 bar, a high-pressure air storage facility (21 tons, 250 bar, 40 kg / s), a storage facility for other gases (oxygen, hydrogen, methane, propane, nitrogen) and a distribution network for water (several tens of liters per second up to 30 bar) and kerosene (3.5 L / s up to 80 bar).... |
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| 7. | PIV at ONERA DAFE : equipment - ONERA / DAFE-EN |
| | Hot flows (T 100 °C) and/or high-pressure flows (p 20 bar) :... Solid magnesium oxyde or titanium oxyde particles, injected with low and high pressure cyclone aerosol generators.... |
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| 8. | Aerothermodynamics - ONERA / DAAP-EN |
| | Migration of Hot Spots in a High Pressure Turbine... A 3D unsteady numerical simulation was performed using Navier-Stokes equations of the case of a high pressure turbine stage to model the temperature distortions (hot spots) on the turbine inlet.... |
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| 9. | LACOM - The Multiphase Combustion Laboratory - ONERA / DMAE-EN |
| | Improve the performance of aircraft engines : higher compression pressure and turbine entry temperature, to increase efficiency and reduce specific fuel consumption.... |
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| 10. | Launchers (LANC3) |
| | These may be later used in more severe conditions, i.e. higher pressures and flow rates on the P8 test facility at DLR / Lampoldshausen.... |
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