EDITH
Soufflerie pour l’Étude Des Interactions et Transferts en Hypersonique
Wind Tunnel for the Study of Interactions and Transfers in Hypersonicity
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Contact : Viviana LAGO
Principal features
Long service life 20 minutes Experimental chamber: cylindrical L 1,2m x D 1,7m Nozzle: with adaptated contour and adaptable conicals on request |
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Pumping unit capacity : 9000 m3/h Statistical pressure, Pa : 8.103 Stop pressure, Pa : 3.105 Mach number : 3 Reynolds number/m : Re = 2,77.107 Gaz : air tank at 300 Bar |
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The operating conditions can be adapted according to the nozzle |
Model
Scope, cm < 10
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Applications and research areas
Fundamental shockwave research
Aerodynamic and aerothermal behaviour of probes and spacecraft
Fluidic vectoring.of supersonic flows