The system of complex automation of aerodynamic experiment in T-106 TsAGI transonic wind tunnel is presented. Data acquisition processes, as well as control processes for the model's Mach number and angle of attack are automated on the basis of new data acquisition and control system involving IVK M2 data acquisition software package and VMIC control software package. The results of balance and pressure experiments (and of the combined ones) are presented. Stages of experimental results processing are described.
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