CFD Analysis of UAV Flying Wing

2016 INCAS Bulletin  
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.
doi:10.13111/2066-8201.2016.8.3.6 fatcat:fkme5kzdevf2jiagwbkywgz2pq