This study investigates the effects of aerodynamic interaction on the aeroelastic
characteristics of wings in proximity which is considered to be aerodynamically more …

The joined-wing aircraft is an alternative configuration compared to general cantilevered
configuration because of its superiority. In the present work, an efficient modeling method for …

This paper presents a new‐concept aircraft with a diamond joined‐wing morphing
configuration, which simultaneously adjusts the sweep angles of both the front wing and rear …

This paper investigates the aeroelastic behavior of elastically supported airfoils due to
structural and aerodynamic coupling effects between them in an incompressible uniform …

A novel mechanism is described that increases the critical buckling load of the rear wing of
joined-wing aircraft in an effort to reduce structural weight. The benefits of the joined-wing …

The basic understanding of the significance of aircraft loads and their relationship to
aeroelasticity will be elaborated comprehensively. The estimation of loads acting on an …

This chapter intends to aid the world of Internet of Drones by increasing the flight time of the
UAV systems via modifying the winglet. This modification was done in a hybrid VTOL UAV to …

The presented work aims to showcase a joined-wing (JW) concept with key design
parameters based on the NASA Common Research Model (CRM) configuration, to highlight …

I. INTRODUCTION The Blended-Wing-Body (BWB) aircraft concept blends the fuselage,
wing, and the engines into a single lifting surface, allowing the aerodynamic efficiency to be …

Anticipating potentialair transportation markets in the business jet type, the present work is
devoted for exploring the possibilities of introducing some of a number of visionary and …