CFD Analysis of UAV Flying Wing
Journal Title: INCAS BULLETIN - Year 2016, Vol 8, Issue 3
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.
Authors and Affiliations
Vasile PRISACARIU
Keywords
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- EP ID EP118143
- DOI 10.13111/2066-8201.2016.8.3.6
- Views 112
- Downloads 0
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