| 1. | JSO AppUn de Saint-Victor |
| | LF... |
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| 2. | Modeling and Simulating Medium and High Frequency Vibrations of Complex Structures - ONERA / DADS-EN |
| | Their dynamics are physically well represented by global standing waves (the eigenmodes) in the low-frequency (LF) range.... But this approach fails dramatically as frequency increases because of the multiple interactions of waves with material heterogeneities at the wavelength scale, and reflections on boundaries and at interfaces between structural elements with different stiffnesses (stiffeners on plates and shells, bulkheads, stringers, etc.). In the " intermediate " or mid-frequency (MF) range, a transition zone between the LF and HF behaviours is observed.... |
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| 3. | Internal Noise Prediction in Fixed-Wing Aircraft Fuselages - ONERA / DADS-EN |
| | Fixed-Wing Aircrafts and Helicopters :Internal Vibroacoustics in the LF, MF and HF Range. Internal Noise Prediction of Internal Noise in Fixed-Wing Aircraft Fuselages. The DADS department at ONERA is involved in the development of numerical tools for the prediction of internal noise in aerospace structures.. |
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| 4. | A cryogenic combustion research test bench - Operation with Oxygen / Hydrogen - ONERA / DEFA-EN |
| | These experiments, conducted with various Onera and CNRS teams, can be classified with respect to the phenomenon being studied : atomization, vaporization, turbulent combustion, stability (LF and HF), ignition, and heat transfers.... |
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| 5. | 08-Presteau.pdf |
| | Le lf ls... |
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| 6. | No title |
| | I. 3D Flow in frame rotating at rate Rossby number Ro = U / (Lf), where f = 2 II. Flow on the - plane Rhines number Rh = U / (L2), where f = 2 + y, and is the latitude variation of the Coriolis parameter f A reduced model of near-resonant triads captures self-organization of small-scale fluctuations into vor tical columns in 3D zonal flows on the - plane - p. 3/2... |
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