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Improvements to the aircraft Euler methodAn unstructured mesh of tetrahedra offers an attractive approach to mesh generation for complex three dimensional shapes. The combination of a method for constructing tetrahedral meshes and a finite element technique for solving the Euler equations has resulted in a powerful new approach to the problem of calculating flows over complex geometries. Recent progress and improvements to the authors' aircraft Euler method are described and results presented to demonstrate its capability.
Document ID
19870035370
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jameson, A.
(Princeton Univ. NJ, United States)
Baker, T. J.
(Princeton University NJ, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 87-0452
Report Number: AIAA PAPER 87-0452
Accession Number
87A22644
Distribution Limits
Public
Copyright
Other

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