01.2 - Aircraft Design and Integrated System (Applications)
RESEARCH ON THE OVERALL DESIGN OF A HIGH-SPEED MORPHING UAV
C. Ding, School of Aeronautic Science and Engineering,Beihang University, China; T.-L. Ma, Institute of Unmanned System, Beihang University, China; J.-C. Fu, School of Transportation ScienceandEngineering,BeihangUniversity, China; X.-S. Wang, School of Aeronautic Science and Engineering, Beihang University, China
This paper takes the air-launch high-speed aircraft with the morphing wing as the research object, carries out the overall design research according to the proposed task requirements, forms the calculation method of the overall parameters of the variant high-speed aircraft, and proposes a variable outer wing aerodynamic layout form.