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NASA NTRS · 19870016562

Transonic flow solutions using a composite velocity procedure for potential, Euler and RNS equations

Abstract

Solutions 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.

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BibTeXRIS

Gordnier, R. E., Rubin, S. G.. 1986-01-01. Transonic flow solutions using a composite velocity procedure for potential, Euler and RNS equations. https://ntrs.nasa.gov/citations/19870016562

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