25th Congress of International Council of the Aeronautical Sciences, 3 - 8 September 2006, Hamburg, Germany
Paper ICAS 2006-3.2.1


SUMMARY OF THE DYNAMIC TEST CAPABILITIES AT CARIA LOW SPEED WIND TUNNEL

X. Q. Du, W. D. Hao, C. Bu
China Aerodynamics Research Institute of Aeronautics, China

Keywords: Dynamic Wind Tunnel Test, Rotary Balance, Forced oscillation, Maneuver Simulation

A summary is presented of CARIA’s dynamic test capability in FL-8 low speed wind tunnel. CARIA has developed four sets of apparatus to study the dynamic stability characteristics and the unsteady and non-linear aerodynamic characteristics of an airplane flying at high angle of attack and high angular rate.


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