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.
Three-Dimensional, Subsonic, Turbulent Juncture Region Flow
NASA Tech Briefs ; 9 , 4
01.03.1986
Sonstige
Keine Angabe
Englisch
Turbulent flow around a wing-fuselage type juncture
AIAA | 1985
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