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Adaptive computational methods for aerothermal heating analysisThe development of adaptive gridding techniques for finite-element analysis of fluid dynamics equations is described. The developmental work was done with the Euler equations with concentration on shock and inviscid flow field capturing. Ultimately this methodology is to be applied to a viscous analysis for the purpose of predicting accurate aerothermal loads on complex shapes subjected to high speed flow environments. The development of local error estimate strategies as a basis for refinement strategies is discussed, as well as the refinement strategies themselves. The application of the strategies to triangular elements and a finite-element flux-corrected-transport numerical scheme are presented. The implementation of these strategies in the GIM/PAGE code for 2-D and 3-D applications is documented and demonstrated.
Document ID
19880019731
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Price, John M.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Oden, J. Tinsley
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1988
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.26:181636
LMSC-HEC-TR-F225772
NASA-CR-181636
Report Number: NAS 1.26:181636
Report Number: LMSC-HEC-TR-F225772
Report Number: NASA-CR-181636
Accession Number
88N29115
Funding Number(s)
PROJECT: RTOP 506-43-31-03
CONTRACT_GRANT: NAS1-17894
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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