Conceptual Design of a Nonconstant Swept Flying Wing Unmanned Combat Aerial Vehicle
Sign Up to like & getrecommendations! Published in 2023 at "Journal of Aircraft"
DOI: 10.2514/1.c037257
Abstract: The design of unmanned combat aerial vehicles (UCAVs) is primarily governed by the low-observability requirement for military applications rather than aerodynamic performance. The conceptual design and optimization of UCAV models via size and shape variables… read more here.
Keywords: combat aerial; conceptual design; design nonconstant; flying wing ... See more keywords