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Lifting Rotors
 Testing of rotor large-scale models with diameter up to 5m over the speed range from 0 to 430 km/h in the T-104 wind tunnel with test section of 7m in diameter.  Testing of large-scale rotorcraft models with rotor diameter about 4-5m in the T-104 wind tunnel.  Study of aerodynamic and aeroelastic characteristics of full-scale rotor with diameter up to 17m in the T-101 wind tunnel with 14x24m test section.  Aerodynamic characteristics of tilt rotors and wind-wheels are determined in the T-101 and T-104 wind-tunnel.  Development of the fuselage aerodynamic configuration and study of rotor /fuselage models interaction is conducted in the T-105 wind-tunnel with 4.5m test section diameter. /span> |
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© 2012 by TsAGI |
© 2012 by TsAGI |