CFD Analysis of UAV Flying Wing
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 experi...
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National Institute for Aerospace Research “Elie Carafoli” - INCAS
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doaj-1da51e492f7e430ca843f780941abf6c2020-11-24T23:24:35ZengNational Institute for Aerospace Research “Elie Carafoli” - INCASINCAS Bulletin2066-82012247-45282016-09-0183657210.13111/2066-8201.2016.8.3.6CFD Analysis of UAV Flying WingVasile PRISACARIU0“Henri Coandă” Air Force Academy of Braşov, Romania, Mihai Viteazul, nr. 160, Brasov 500187, Romania, aerosavelli73@yahoo.comNumerical 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.http://bulletin.incas.ro/files/prisacariu__vol_8_iss_3.pdfmesh networksCFD analysisUAVflying wing |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Vasile PRISACARIU |
spellingShingle |
Vasile PRISACARIU CFD Analysis of UAV Flying Wing INCAS Bulletin mesh networks CFD analysis UAV flying wing |
author_facet |
Vasile PRISACARIU |
author_sort |
Vasile PRISACARIU |
title |
CFD Analysis of UAV Flying Wing |
title_short |
CFD Analysis of UAV Flying Wing |
title_full |
CFD Analysis of UAV Flying Wing |
title_fullStr |
CFD Analysis of UAV Flying Wing |
title_full_unstemmed |
CFD Analysis of UAV Flying Wing |
title_sort |
cfd analysis of uav flying wing |
publisher |
National Institute for Aerospace Research “Elie Carafoli” - INCAS |
series |
INCAS Bulletin |
issn |
2066-8201 2247-4528 |
publishDate |
2016-09-01 |
description |
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. |
topic |
mesh networks CFD analysis UAV flying wing |
url |
http://bulletin.incas.ro/files/prisacariu__vol_8_iss_3.pdf |
work_keys_str_mv |
AT vasileprisacariu cfdanalysisofuavflyingwing |
_version_ |
1725559983901245440 |