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On the vortical-flow-prediction capability of an unstructured-grid Euler solverThe results from a concentrated computational effort are presented with the primary objective being directed at evaluating the vortical-flow-prediction capability of an unstructured-grid Euler solver. Both viscous and inviscid solutions, obtained from an established structured-grid method, along with experimental wind-tunnel data are used as benchmark measures to assess the validity of the unstructured-grid Euler results. Viscous effects on vortical flows are first identified by comparing the viscous and inviscid solutions obtained from the structured-grid method. Computational data analysis is then presented which reveals excellent correlations between the inviscid structured and unstructured-grid results in terms of off-surface flow structures, surface pressure distribution, and the predicted longitudinal aerodynamic characteristics. The sensitivity of the unstructured-grid inviscid solutions to grid refinement is also discussed along with an analysis of the convergence and performance characteristics for each method.
Document ID
19980028360
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Farhad Ghaffari ORCID
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
August 17, 2013
Publication Date
January 10, 1994
Publication Information
Publication: 32nd Aerospace Sciences Meeting and Exhibit
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Fluid Mechanics and Thermodynamics
Report/Patent Number
AIAA-94-0163
Report Number: AIAA Paper 94-0163
Meeting Information
Meeting: 32nd Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: US
Start Date: January 10, 1994
End Date: January 13, 1994
Sponsors: American Institute of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Unstructured grid
Aerodynamic characteristics
Vortex structure
Reynolds Averaged Navier Stokes
Wind tunnel models
High aspect ratio
Aerodynamic performance
Fuselage station
Static pressure
Data analysis
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