03.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
EVALUATION OF CONCEPTUAL DESIGN BASED ON MANUFACTURED ACTUAL UNMANNED SOLAR PLANE
N. Araiš, W. Harasani, King Abdruaziz Univ., Saudi Arabia; K. Hiraokaš; šTokai Univ., Japan
In order to verify the long-endurance flight as aim of multiple-days, we developed an unmanned solar plane that has 7.6m span main wing and GaAs modules, and conceptual design method was modified by results of manufacturing and test flight so as to evaluate the mass of airframe and required power more accurately.