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CFD Process Automation Using Overset GridsThis talk summarizes three applications of the overset grid method for CFD using some level of automated grid generation, flow solution and post-processing. These applications are 2D high-lift airfoil analysis (INS2D code), turbomachinery applications (ROTOR2/3 codes), and subsonic transport wing/body configurations (OVERFLOW code). These examples provide a forum for discussing the advantages and disadvantages of overset gridding for use in an automated CFD process. The goals and benefits of the automation incorporated in each application will be described, as well as the shortcomings of the approaches.
Document ID
20020034859
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Buning, Pieter G.
(NASA Ames Research Center Moffett Field, CA United States)
George, Michael W.
Date Acquired
August 20, 2013
Publication Date
January 1, 1995
Subject Category
Fluid Mechanics And Thermodynamics
Meeting Information
Meeting: NASA Workshop on Surface Modeling, Grid Generation, and Related Issues in CFD Solutions
Location: Cleveland, OH
Country: United States
Start Date: May 9, 1995
End Date: May 12, 1995
Sponsors: NASA Headquarters
Funding Number(s)
PROJECT: RTOP 505-59-53
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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