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Three-dimensional implicit lambda methodsThis paper derives the three dimensional lambda-formulation equations for a general orthogonal curvilinear coordinate system and provides various block-explicit and block-implicit methods for solving them, numerically. Three model problems, characterized by subsonic, supersonic and transonic flow conditions, are used to assess the reliability and compare the efficiency of the proposed methods.
Document ID
19840006055
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Napolitano, M.
(NASA Langley Research Center Hampton, VA, United States)
Dadone, A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
October 1, 1983
Subject Category
Aerodynamics
Report/Patent Number
REPT-83-62
NASA-CR-172264
NAS 1.26:172264
Report Number: REPT-83-62
Report Number: NASA-CR-172264
Report Number: NAS 1.26:172264
Accession Number
84N14123
Funding Number(s)
CONTRACT_GRANT: NAS1-17070
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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