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CFD Analysis of UAV Flying Wing
oleh: Vasile PRISACARIU
Format: | Article |
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Diterbitkan: | National Institute for Aerospace Research “Elie Carafoli” - INCAS 2016-09-01 |
Deskripsi
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.