I’ve the hand-made aircraft structure which upper wing model.
Wing span 3.16m
airframe weight 10 kg
airfoil: CLARK Y AIRFOIL (clarky-il)
So, how can I choose the propulsion for vertical and forward flight?
I’ve the hand-made aircraft structure which upper wing model.
Wing span 3.16m
airframe weight 10 kg
airfoil: CLARK Y AIRFOIL (clarky-il)
So, how can I choose the propulsion for vertical and forward flight?