Wind tunnel T-106
Basic parameters
| Flow Mach number | 0.15–1.1 |
| Reynolds number per 1 m | up to 35∙106 |
| Total pressure | 50–500 kPa |
| Dynamic pressure | up to 58 kPa |
| Stagnation temperature | 290–330 К |
| Angle of attack (α): | |
| Electric-mechanical balance | –10°–40° |
| In-model strain-gauge balance | 0°–90° |
| Model dimensions: | |
| Wing span | up to 1.7 m |
| Length | up to 2.2 m |
| Wing area | up to 0.5 m2 |
| Model weight | up to 250 kg |
| Test section dimensions: | |
| Cross section diameter | 2.48 m |
| Test section length | 4.85 m |
| Porosity coefficient of test section walls | 15% |
General description
T-106 is a close-layout, continuous-operation, variable-density wind tunnel designed for investigating aerodynamic characteristics of aircraft models and flight vehicle components at subsonic and transonic velocities. The flow is generated by a compressor with an electric drive of 32 MW.
Test section with a circular cross-section and perforated walls is equipped with an electric-mechanical balance and a set of in-model strain-gauge balances for measuring aerodynamic forces and moments of models and their elements, and with supporting devices of 3 types (strip suspension, tail sting and under-fuselage strut).
The wind tunnel is equipped with automated computation and measurement complex for data monitoring, registration, acquisition, and processing during the experiment.
Capabilities
- electric-mechanical and strain-gauge balance measurements of total aerodynamic characteristics of aircraft models and their elements;
- measurement of pressure distribution along the model surface using electronic pressure modules for 1000 points;
- determination of characteristics of inlet models and aircraft models with the flow passing through the internal channels of thenacelles;
- investigation of the models with simulation of the high-pressure jets (power plant nozzles, including those of variable thrust vector,jet flaps, etc.;
- investigation of characteristics of aircraft models static and dynamic aeroelasticity;
- test of half-models on a special supporting device;
- investigation of wing profiles;
- physical investigations.
Practical application
During 70 years T-106 has been one of the most loaded TsAGI’s facilities for investigating different-application flight vehicles at high subsonic and transonic velocities.