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Modularization and Validation of FUN3D as a CREATE-AV Helios Near-Body SolverUnder a recent collaborative effort between the US Army Aeroflightdynamics Directorate (AFDD) and NASA Langley, NASA's general unstructured CFD solver, FUN3D, was modularized as a CREATE-AV Helios near-body unstructured grid solver. The strategies adopted in Helios/FUN3D integration effort are described. A validation study of the new capability is performed for rotorcraft cases spanning hover prediction, airloads prediction, coupling with computational structural dynamics, counter-rotating dual-rotor configurations, and free-flight trim. The integration of FUN3D, along with the previously integrated NASA OVERFLOW solver, lays the ground for future interaction opportunities where capabilities of one component could be leveraged with those of others in a relatively seamless fashion within CREATE-AV Helios.
Document ID
20160007705
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Jain, Rohit
(Army Research Development, and Engineering Command Moffett Field, CA, United States)
Biedron, Robert T.
(NASA Langley Research Center Hampton, VA, United States)
Jones, William T.
(NASA Langley Research Center Hampton, VA, United States)
Lee-Rausch, Elizabeth M.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
June 20, 2016
Publication Date
January 4, 2016
Subject Category
Aircraft Design, Testing And Performance
Computer Programming And Software
Report/Patent Number
NF1676L-22526
Report Number: NF1676L-22526
Meeting Information
Meeting: 2016 AIAA Science and Technology Forum and Exposition
Location: San Diego, CA
Country: United States
Start Date: January 4, 2016
End Date: January 8, 2016
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 109492.02.07.01.02.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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