Conceptual Design of a Nonconstant Swept Flying Wing Unmanned Combat Aerial Vehicle

What is it about?

The conceptual design of present UCAVs lies between the fighter and the bomber. However, the configurations of UCAV are still under exploration and undergoing various developments, so the standard dimensions and shapes of the UCAV design have not been defined yet. Hence, assessing the conceptual configurations and their design are worthy issues that need to be investigated. This research discusses the preliminary conceptual design and optimization of a UCAV configuration with a non-constant leading-edge sweep angle.

Featured Image