Publication Date:
2019-06-28
Description:
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.
Keywords:
MECHANICS
Type:
LAR-13263
,
NASA Tech Briefs (ISSN 0145-319X); 9; 4; P. 150
Format:
text
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