| 1. | Soufflerie pour l'étude des sites industriels et urbains - Offre technologique Onera |
| | Wind tunnel well adapted for the study of complete urban and industrial sites with simulations of wind flow boundary layers.... |
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| 2. | Wind Tunnel for the Study of Industrial and Urban Sites - Onera's Technological Offer |
| | Wind tunnel well adapted for the study of complete urban and industrial sites with simulations of wind flow boundary layers.... |
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| 3. | ONERA - Fundamental and Experimental Aerodynamics (DAFE) - References |
| | Fine grain description of separated flows, shock wave / boundary layer interactions and vortex structures... |
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| 4. | DAFE Computation Codes - ONERA / DAFE-EN |
| | Boundary layer type codes for rapid evaluation of turbulent boundary layers.... |
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| 5. | Fundamental and Experimental Aerodynamics - ONERA / DAFE |
| | In priority, the work covers : separated turbulent flows, the formation and development of vortexes shock phenomena, in particular, shock interferences and shock wave / boundary layer interactions, turbulence, unsteady effects and instabilities in free flowsz... Control of Shock Wave / Boundary Layer Interactions... |
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| 6. | Boundary Layer Computations with the 3C3D Code - ONERA / DMAE-EN |
| | Boundary Layer Computations with the 3C3D Code - ONERA / DMAE-ENWho are we ?Aerodynamics and Energetics Modeling... Boundary Layer Computations with the 3C3D Code. 3D computation of boundary layer turbulence on a cruciform missile. The surface heat flux of profiled bodies in non-separated flow can be found from the velocity field of an ideal fluid at the surface by solving the boundary layer equations, which is often a simpler procedure than a full Navier-Stokes computation.. |
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| 7. | L2 Site Wind Tunnel - ONERA / DAAP-EN |
| | A grid can be introduced to simulate the atmospheric boundary layer over the site, by deforming the vertical velocity gradient.... |
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| 8. | Transonic Flow around Fuselage and Wings - ONERA's Science Pictures |
| | Manoeuvring in such conditions might increase the shock, causing the rise of pressure gradient and the separation of the boundary layer.... |
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| 9. | Conference - Turbulence and Interactions - Porquerolles - 29 May - 2 June 2006 |
| | Objectives and challenges for the problem of unsteadiness in shock boundary layer interactions... Compressible turbulent boundary layers with non-adiabatic walls "... |
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| 10. | Stemmer.dvi |
| | Complex flow phenomena like shock / boundary-layer interactions and the simulation of reacting flows require careful attention to the numerical method and require fine enough resolution to calculate all necessary physical effects properly.... Hypersonic reacting flat-plate boundary-layer flow... BIBLIOGRAPHY [ 12 ] L.M Mack, " Boundary-Layer Stability Theory ", JPL Report 900-277 Rev A, Jet Propulsion Laboratory, Pasadena, USA, 1969. [ 13 ] S.G. Mironov and A.A Maslov, " Experimental study of secondary stability in a hypersonic shock layer on a flat plate ".... |
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