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 95
  • Downloads 0

How To Cite

Vasile PRISACARIU (2016). CFD Analysis of UAV Flying Wing. INCAS BULLETIN, 8(3), 65-72. https://europub.co.uk/articles/-A-118143