NASA NTRS · 19910011780
Solution of three-dimensional afterbody flow using reduced Navier-Stokes equations
Abstract
The flow over afterbody geometries was investigated using the reduced Navier-Stokes (RNS) approximation. Both pressure velocity flux-split and composites velocity primitive variable formulations were considered. Pressure or pseudopotential relaxation procedures are combined with sparse matrix or coupled strongly implicit algorithms to form a three-dimensional solver for general non-orthogonal coordinates. Three-dimensional subsonic and transonic viscous/inviscid interacting flows were evaluated. Solutions with and without regions of recirculation were obtained.
Keep this discovery
Explore connections, maps & timelines
Almahroos, H. M. H., Khosla, P. K., Rubin, S. G.. 1991-01-01. Solution of three-dimensional afterbody flow using reduced Navier-Stokes equations. https://ntrs.nasa.gov/citations/19910011780
Cite the original work for its findings. Save a collection to share your selection of sources.