03.2 - Experimental Aerodynamics
DESIGN OF DUAL-FUSELAGE FLIGHT PLATFORM FOR JET CONTROL FUNCTION VERIFICATION
C.P. Li, China; G. Zhang, China; N. Liu, China; Y. Zhang, China; L. Xu, China; M. Wang, China
At present, the numerical simulation and wind tunnel test methods used in the study of jet control mechanism are relatively mature, but the means for systematic verification are generally lacking. For this purpose, this paper proposes a low-cost flight platform which can verify the autonomous jet control function in the air.