01 - Aircraft Design and Integrated Systems
OPTIMIZATION OF MOTOR FOR THE MAXIMIZATION OF SOLAR-POWERED AIRCRAFT PERFORMANCE
S. Serokhvostov, MIPT, Russia; T. Churkina, MAI, Russia
The problem of energy saving through the moto maximal power restriction for the solar-powered airplane is investigated. Based on the previous results the model of this phenomenon was formed. Numerical results for artificial plane were obtained. Analytical results were compared with numerical ones and have shown acceptable accuracy.