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Demonstration of an automated CFD system for three-dimensional flow simulationsIn this paper the capabilities of an automated CFD system which is currently available at NLR are demonstrated. Transonic flow around the AS28G wing/body configuration and hypersonic flow through a generic three-dimensional mixed-compression airbreathing inlet are simulated. An assessment of the level of automation of the current CFD-system is made. The problem-turnaround time lies within the order of a week for both applications.
Document ID
19950022346
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Vanderburg, J. W. (National Aerospace Lab. Amsterdam, Netherlands)
Maseland, J. E. J. (National Aerospace Lab. Amsterdam, Netherlands)
Hagmeijer, R. (National Aerospace Lab. Amsterdam, Netherlands)
Decock, K. M. J. (National Aerospace Lab. Amsterdam, Netherlands)
Date Acquired
September 6, 2013
Publication Date
March 1, 1995
Publication Information
Publication: NASA. Lewis Research Center, Surface Modeling, Grid Generation, and Related Issues in Computational Fluid Dynamic (CFD) Solutions
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
95N28767
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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