01 - Aircraft Design and Integrated Systems
GENERAL PARAMETERS DESIGN METHOD OF CANARD ROTARY WING AIRPLANE UNDER THE INFLUENCE OF POWER SYSTEM
Y. Na, School of Aeronautics Northwestern Polytechnical University, China; Z.-H. Gao¹, Y.-P. Deng¹, L. Tian¹, H.-G. Gao¹; ¹School of Aeronautics Northwestern Polytechnical University, China
The power demand of canard rotary wing airplane’s helicopter mode and fixed wing mode are different,it will influence the fuel consumption and stability of the engine.The paper introduces a method to comprehensive design the general parameters of the aircraft's fixed wing mode and helicopter mode combined with engine characteristics.The method is also suitable for other types of VTOL.