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A Selection of Experimental Test Cases for the Validation of CFD Codes, Volume 2This report presents the results of a study by Working Group 14 of the AGARD Fluid Dynamics Panel. The thirty nine test cases that are documented cover the subsonic, transonic, and supersonic flow regimes and five classes of geometries. Included in the five classes of geometries are: Two Dimensional Airfoils; Three Dimensional Wings, designed for predominantly attached flow conditions; Slender Bodies, typical of missile type configurations; Delta Wings, characterized by a conical type of vortex flow; and Complex Configurations, either in a geometrical sense or because of complicated flow interactions. The report is presented in two volumes. Volume 1 provides a review of the theoretical and experimental requirements, a general introduction, summary of the test cases and recommendations for the future. Volume 2 contains detailed information on the test cases.
Document ID
19950011431
Acquisition Source
Legacy CDMS
Document Type
Other - Collected Works
External Source(s)
https://www.sto.nato.int/publications/AGARD/AGARD-AR-303-VOL-2/AGARD-AR-303-Vol-2.pdf
Authors
Advisory Group for Aerospace Research and Development (North Atlantic Treaty Organization Brussels, Belgium)
Date Acquired
August 16, 2013
Publication Date
January 8, 1994
Publication Information
Publication: A Selection of Experimental Test Casesfor the Validation of CFD Codes
Publisher: AGARD
Volume: 2
Issue: 303
Issue Publication Date: January 8, 1994
ISBN: 92-836-1003-2
Subject Category
Aerodynamics
Report/Patent Number
AGARD-AR-303-VOL-2
ISBN: 92-836-1003-2
Report Number: AGARD-AR-303-VOL-2
Accession Number
95N17846
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
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