NASA NTRS · 19850000540
Three-Dimensional, Subsonic, Turbulent Juncture Region Flow
Abstract
CMC3DPNS predicts three-dimensional, subsonic, turbulent aerodynamic juncture region flow. Versatile program for comprehensive flow-field analysis applies finite-element methodology to nonlinear field problems. Order-ofmagnitude analysis of subsonic, three-dimensional, steady time-averaged NavierStokes equations for semibounded aerodynamic juncture geometries yields para bolic Navier-Stokes equations. CMC3DPNS solves these equations to predict juncture-region flow.
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Baker, A. J., Manhardt, P. D., Orzechowski, J. A.. 1986-03-01. Three-Dimensional, Subsonic, Turbulent Juncture Region Flow. https://ntrs.nasa.gov/citations/19850000540
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