Innovation design analysis of the optimal aerodynamic adaptive smart structures for disk-body solar Hybrid Electric aircraft and airship concepts

Abstract

The innovation integrated design analysis of the concept of finding any optimal aerodynamic structure with adaptive intelligent systems as a means of changing facility of the geometric shape of the surface by integrating the disc wing-body of a solar Hybrid Electrical aircraft (HEA) and an airship to reduce weight, power and fuel sources is very relevant today and focused on the international research EC programs of future green ecology air transportation. The universal digital method for optimizing the CAD aircraft design is presented which is focused on achieving the goal of minimum weight-drag-frontal stability of the layout from the virtual center of mass allows us to get the layout of the aircraft from the conditions of reducing the time of full flight operation of E-Mobility and low cost for priority with realize a short take-off and landing (STOL) with high angle of the flight path and compact infrastructural restrictions in the terminal slot configurations of modern urban airport infrastructure and achieving zero toxic & noise regulation by IATA/ICAO. The joint results of EC international R&D collaboration to accelerate the synergy effect of new aircraft concepts.