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Unstructured grid solutions to a wing/pylon/store configuration using VGRID3D/USM3DThe purpose of this paper is to validate an inviscid flow solution package based on a new unstructured grid methodology using experimental data on a wing/pylon/store configuration. The solution package consists of an advancing front unstructured grid generator, VGRID3D, and an efficient Euler equation solver, USM3D. Comparisons of computed data versus experimental data are made for two free-stream Mach numbers at five store locations relative to the wing. Both rigid body aerodynamics and mutual interference effects are explored. A very good agreement is observed between computed and wind tunnel data.
Document ID
19930029306
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Parikh, Paresh
(NASA Langley Research Center Hampton, VA, United States)
Pirzadeh, Shahyar
(Vigyan, Inc. Hampton, VA, United States)
Frink, Neal T.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 15, 2013
Publication Date
August 1, 1992
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 92-4572
Meeting Information
Meeting: AIAA, Atmospheric Flight Mechanics Conference
Location: Hilton Head Island, SC
Country: United States
Start Date: August 10, 1992
End Date: August 12, 1992
Sponsors: AIAA
Accession Number
93A13303
Funding Number(s)
CONTRACT_GRANT: NAS1-18585
Distribution Limits
Public
Copyright
Other

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