| 1. | ONERA - Aérodynamique fondamentale et expérimentale (DAFE) - Publications |
| | Design of a boundary layer suction device for a supersonic quiet wind tunnel by numerical simulation, Aerospace Science and Technology-AST, 8 (2004), Elsevier, pp.... |
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| 2. | ONERA - Fundamental and Experimental Aerodynamics (DAFE) - Facilities |
| | Spearheading advances in aerodynamics implies synergy between three components : research teams, metrology methods and test facilities.The Department's test resources incorporate a full line of research wind tunnels covering the entire Mach range from 0 to 10 (subsonic, transonic, supersonic and so-called " cold " hypersonic wind tunnels).. |
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| 3. | ONERA - Fundamental and Experimental Aerodynamics (DAFE) - Publications |
| | Design of a boundary layer suction device for a supersonic quiet wind tunnel by numerical simulation, Aerospace Science and Technology-AST, 8 (2004), Elsevier, pp.... |
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| 4. | Plasmas for Flow Control / Abstracts |
| | The experimental tests are conducted in transonic and supersonic wind tunnels.... |
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