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AIRPLANE: Unstructured-Mesh Applications Douglas Aircraft Company Long Beach, CA

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Vassberg, John C., author.
Conference Name:
Aerospace Technology Conference & Exposition (1990-10-01 : Long Beach, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1990
Summary:
Applications of and recent improvements to the AIRPLANE program (developed by Jameson and Baker) are presented. This unstructured-mesh Euler method is capable of solving the inviscid transonic flow about complex three-dimensional aircraft configurations. Preliminary validations for the ONERA-M6 wing are made with comparisons to test data and a structured-mesh Euler code. Geometric capabilities of the present method are illustrated with solutions about simple, semi-complex and extremely complex aerodynamic configurations. Post-processing techniques for unstructured-mesh solutions are also presented. Computational resources and manpower requirements are benchmarked for the ONERA-M6 wing and a generic MDC Tri-Jet transport; the computers utilized for this survey include CONVEX, CRAY, Hitachi and IBM
Notes:
Vendor supplied data
Publisher Number:
901857
Access Restriction:
Restricted for use by site license

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