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A semi-direct solver for compressible 3-dimensional rotational flowAn iterative procedure is presented for solving steady inviscid 3-D subsonic rotational flow problems. The procedure combines concepts from classical secondary flow theory with an extension to 3-D of a novel semi-direct Cauchy-Riemann solver. It is developed for generalized coordinates and can be exercised using standard finite difference procedures. The stability criterion of the iterative procedure is discussed along with its ability to capture the evolution of inviscid secondary flow in a turning channel.
Document ID
19830026637
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Chang, S. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Adamczyk, J. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1983
Subject Category
Aerodynamics
Report/Patent Number
E-1556
NAS 1.15:83314
NASA-TM-83314
Report Number: E-1556
Report Number: NAS 1.15:83314
Report Number: NASA-TM-83314
Accession Number
83N34908
Funding Number(s)
PROJECT: RTOP 505-31-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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