NASA NTRS · 19820034247
A viscous-inviscid interaction algorithm for three-dimensional turbulent subsonic aerodynamic juncture region flow
Abstract
An order-of magnitude analysis of the subsonic, three-dimensional, steady time-averaged Navier-Stokes equations for semibounded aerodynamic juncture geometries yields the parabolic Navier-Stokes simplification. The numerical solution of the resultant pressure Poisson equation is cast into complementary and particular parts, yielding an iterative interaction algorithm with an exterior three-dimensional potential flow solution. A parabolic transverse momentum equation set is constructed, wherein robust enforcement first-order continuity effects is accomplished using a penalty differential constraint concept within a finite element solution algorithm. A Reynolds stress constitutive equation, with low turbulence Reynolds number wall functions, is employed for closure, using parabolic forms of the two-equation turbulent kinetic energy-dissipation equation system. The algorithm is employed to predict the three-dimensional turbulent flowfield in the juncture region formed by two intersecting parabolic arcs at a free-stream Mach-number of 0.08, and Re/C = 600,000/m.
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Baker, A. J., Orzechowski, J. A.. 1982-01-01. A viscous-inviscid interaction algorithm for three-dimensional turbulent subsonic aerodynamic juncture region flow. https://ntrs.nasa.gov/citations/19820034247
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