Wing design for Jet model Dassault FALCON 7X

Abstract

Abstract:  Present-day wing design is more challenging in aerodynamics and there is a need for flights that consume less fuel and the necessity of self-healing for dynamic damages due to bird strikes, turbulence, etc., and aerodynamically improve the performance. Wings should be strong, stiff, durable, and lightweight to withstand aerodynamic forces. A comparative study of the use of variable geometry wings on one of the most famous business jet models, the Dassault Falcon 7X, is presented in this paper to address this problem. Here, the computational program STAR CCM+ CFD solver is used to conduct a comparative aerodynamic study of variable geometry wing advantage in the design of one of the most famous business jet modules Dassault FALCON 7X. The Falcon 7X is chosen in this work because of its structural features such as wings fitted with winglets, windshields, typical landing weight, etc., CFD study is done using self-healing material which can be auto repair under stimulus when the damage or fracture occurs in the time-of-service operation either aging or accidentally.

 Index Terms: Swept wing, FALCON 7X, Super healing materials, CFD study.