DocumentCode
3028365
Title
High fidelity methods and physics for UAV flow regimes
Author
Melville, Reid ; Visbal, Miguel ; Gordnier, Raymond
Author_Institution
Computational Sci. Center, Air Force Res. Lab., Wright-Patterson AFB, OH, USA
fYear
2004
fDate
7-11 June 2004
Firstpage
138
Lastpage
143
Abstract
Planned Air Force Unmanned Air Vehicles (UAVs) will be limited by highly nonlinear flow regimes, so an advanced simulation capability has been applied to this class of problems. The proposed paper will document several large-scale computational studies and efforts to validate and to extend the solver capability.
Keywords
computational fluid dynamics; military aircraft; remotely operated vehicles; weapons; Planned Air Force Unmanned Air Vehicle; UAV flow regime; nonlinear flow regime; Computational modeling; Engines; Filters; Laboratories; Large-scale systems; Military computing; Physics; Scalability; Unmanned aerial vehicles; Weapons;
fLanguage
English
Publisher
ieee
Conference_Titel
Users Group Conference (DOD_UGC'04), 2004
Conference_Location
Williamsburg, VA, USA
Print_ISBN
0-7695-2259-9
Type
conf
DOI
10.1109/DOD_UGC.2004.21
Filename
1420863
Link To Document