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An assessment of the adaptive unstructured tetrahedral grid, Euler Flow Solver Code FELISAA three-dimensional solution-adaptive Euler flow solver for unstructured tetrahedral meshes is assessed, and the accuracy and efficiency of the method for predicting sonic boom pressure signatures about simple generic models are demonstrated. Comparison of computational and wind tunnel data and enhancement of numerical solutions by means of grid adaptivity are discussed. The mesh generation is based on the advancing front technique. The FELISA code consists of two solvers, the Taylor-Galerkin and the Runge-Kutta-Galerkin schemes, both of which are spacially discretized by the usual Galerkin weighted residual finite-element methods but with different explicit time-marching schemes to steady state. The solution-adaptive grid procedure is based on either remeshing or mesh refinement techniques. An alternative geometry adaptive procedure is also incorporated.
Document ID
19950012626
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Djomehri, M. Jahed
(Calspan Corp. Moffett Field, CA., United States)
Erickson, Larry L.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1994
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.60:3526
NASA-TP-3526
A-94147
Report Number: NAS 1.60:3526
Report Number: NASA-TP-3526
Report Number: A-94147
Accession Number
95N19041
Funding Number(s)
PROJECT: RTOP 505-59-20
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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