33th Congress of the International Council of the Aeronautical Sciences

03.2 - Experimental Aerodynamics

DEVELOPMENT AND VERIFICATION OF OSCILLATING BLADE GUST GENERATOR IN LOW-SPEED WIND TUNNEL

C. Bu¹, Z. Ma¹, Y. Zhang¹, L. Li¹; ¹AVIC Aerodynamics Research Institute, China

The composition of the oscillating blade gust generator in FL-10 wind tunnel is discussed. The independent drive of the hydraulic servo oscillating cylinder reduces the installation parts and the coupling vibration between the generator and the wind tunnel. The experimental results show that the generator can simulate the combined motion of multiple waveforms with high performance.


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