2006•Aircraft DesignRequires access

An Analytical Study of Two Aerodynamic Configurations For Low RCS for a Fighter Aircraft

Qiu Ju

Abstract

An analysis of stealth performances for a canard-wing-tailplane configuration and a blended wing-fuselage configuration was conducted.The analysis results showed that the blended wing-fuselage configuration provides a higher lift coefficient,a forward shifted aerodynamic focus,and significantly low RCS.Finally,proposed modifications to the aerodynamic configurations were given.

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Key concepts: Fuselage, Aerodynamics, Wing, Aerospace engineering, Wing configuration, Lift coefficient, Lift (data mining), Engineering