Abstract
Numerical methods for solving equations describing the evolution of 3D fluid experienced a significant development closely related to the progress of information systems. Today, especially in the field of fluid mechanics, numerical simulations allow the study of gas-thermodynamic confirmed by experimental techniques in wind tunnel conditions and actual flight tests for modeling complex aircraft. The article shows a case of numerical analysis of the lifting surface on the UAV type flying wing. Key
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CITATION STYLE
PEPELEA, D., COJOCARU, M.-G., … NICULESCU, M.-L. (2016). CFD ANALYSIS FOR UAV OF FLYING WING. SCIENTIFIC RESEARCH AND EDUCATION IN THE AIR FORCE, 18(1), 171–176. https://doi.org/10.19062/2247-3173.2016.18.1.22
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