Design and Analysis of Double Bobble Cross Section Fuselage Micro-Class Aircraft

Abstract

The applications of micro-class aircraft is increasing day by day and all industrial community which depending on mobility and surveillance are accepting this type of aircrafts. The main objective of this work is to design and fabricate an aircraft that is capable to carry the highest payload fraction possible with lowest empty weight fraction which all industries required today. Bobble Cross Section Fuselage Micro-Class Aircraft carriers more pay load with maximum lift, minimum airplane weight and drag.