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Transonic flow solutions using a composite velocity procedure for potential, Euler and RNS equationsSolutions for transonic viscous and inviscid flows using a composite velocity procedure are presented. The velocity components of the compressible flow equations are written in terms of a multiplicative composite consisting of a viscous or rotational velocity and an inviscid, irrotational, potential-like function. This provides for an efficient solution procedure that is locally representative of both asymptotic inviscid and boundary layer theories. A modified conservative form of the axial momentum equation that is required to obtain rotational solutions in the inviscid region is presented and a combined conservation/nonconservation form is applied for evaluation of the reduced Navier-Stokes (RNS), Euler and potential equations. A variety of results is presented and the effects of the approximations on entropy production, shock capturing, and viscous interaction are discussed.
Document ID
19870016562
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Gordnier, R. E.
(Cincinnati Univ. OH, United States)
Rubin, S. G.
(Cincinnati Univ. OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1986
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-180435
NAS 1.26:180435
Report Number: NASA-CR-180435
Report Number: NAS 1.26:180435
Accession Number
87N25995
Funding Number(s)
CONTRACT_GRANT: NAG1-8
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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