2007•Aircraft DesignRequires access

Application of Flying Wing Configuration to UCAV for Reconnaissance

Liu Yan-hua

Abstract

Advantages in application of flying wing configuration to UCAV for reconnaissance are analyzed.Some major technical issues resulting from the application of flying wing configuration are discussed.Finally,it is suggested that the flying wing configuration is an optimal selection of aerodynamic configuration design of an UCAV for reconnaissance.

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Available abstract

Key concepts: Wing, Wing configuration, Aerospace engineering, Configuration design, Aerodynamics, Fixed wing, Engineering, Aeronautics