000013980 001__ 13980
000013980 005__ 20161115094007.0
000013980 04107 $$aeng
000013980 046__ $$k2016-08-21
000013980 100__ $$aMaye, Ryan
000013980 24500 $$aAVT-251: a parametric study of modified saccon geometry

000013980 24630 $$n24.$$p24th International Congress of Theoretical and Applied Mechanics - Book of Papers
000013980 260__ $$bInternational Union of Theoretical and Applied Mechanics, 2016
000013980 506__ $$arestricted
000013980 520__ $$2eng$$aThe North Atlantic Treaty Organization (NATO) has been tasked with completing a “Multi-Disciplinary design and performance assessment of effective, agile NATO Air Vehicles” which has been denoted the AVT-251 task group [1]. One of the goals of this subgroup, denoted the “Aerodynamic Shaping group”, is to determine how the overall leading edge shape effects the aerodynamic characteristics. This paper presents an initial parametric study focused on mesh development. The tasks were: 1) validate the CFD predictions for the latest unmanned combat aerial vehicle (UCAV) shape against previous experimental results, and 2) design and test a meshing topology to be used for future parametric studies. Preliminary simulations were run at M202 and a = 10° and 14° . Both the lift and drag coefficients correlated very well with previous results and pressure coefficient values were almost identical. The initial success of the simulations allows for continued validation and development of the mesh topology.

000013980 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb.
000013980 653__ $$a

000013980 7112_ $$a24th International Congress of Theoretical and Applied Mechanics$$cMontreal (CA)$$d2016-08-21 / 2016-08-26$$gICTAM2016
000013980 720__ $$aMaye, Ryan
000013980 8560_ $$ffischerc@itam.cas.cz
000013980 8564_ $$s209939$$uhttps://invenio.itam.cas.cz/record/13980/files/PO.FM13-1.11.159.pdf$$yOriginal version of the author's contribution as presented on CD, XMLout( page 1384, code PO.FM13-1.11.159).
000013980 962__ $$r13812
000013980 980__ $$aPAPER