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| Description | Subsonic Wind Tunnel: • Prandtl type, horizontal single return • Closed test section, atmospheric • Test section size: 2.5 m wide by 2 m high • Speed range: from 7 to 110 m/s • Angle of attack range: -45º to +45º • Yaw angle range: -140º to +216º • Reynolds number (for ): up to 1x106 • Contraction area ratio: k = 10 • Turbulence factor: 1.11 Trisonic Wind Tunnel • blowdown type • 1.2m x 1.2m test sections (3D) • Mach number range : 0.1 … 3.5 • Reynolds number up to 100 millions/m • Max test run duration : 90 sec. • Max pressure : 12 bar (settling chamber) • Interchangeable porous transonic test section • Variable porosity from 0.01% up to 9% • Interchangeable 3D/2D 0.48m x 1.2m test section • Active model/combustion capability |
| URL | http://www.incas.ro/ |
| Status | Operational since 1901 |
| Scientific Domains | Energy |
| RI Categorization | Civil Engineering Research Infrastructures |
| Location | 220, Iuliu Maniu Boulevard, Bucharest, 061126, Romania |
| MERIL URL | http://portal.meril.eu/meril/view/facilitys/15775 |
