Critical Analysis of a Blended Body Aircraft

Abstract

The blended body aircraft concept is extremely fuel efficient along with other benefits. Flying airplanes to high altitudes requires high lift arising need of better design, increased wingspan and reduced drag. Aircraft with Blended wing body suit the need to fly at high altitudes. It has better stealth properties due to the triangular shape. This study is related to the investigation of a concept airplane by changing the design parameters. Analysis has been done using designing softwares CREO & ANSYS.