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
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;
Conference_Titel :
Users Group Conference (DOD_UGC'04), 2004
Conference_Location :
Williamsburg, VA, USA
Print_ISBN :
0-7695-2259-9
DOI :
10.1109/DOD_UGC.2004.21
