OVERFLOW 2: Overset Grid Computational Fluid Dynamics Flow Solver with Moving Body Capability (OVERFLOW)(LAR-19668-1)

aeronautics
OVERFLOW 2: Overset Grid Computational Fluid Dynamics Flow Solver with Moving Body Capability (OVERFLOW)
(LAR-19668-1)
Overview
OVERFLOW 2 is a computer code for simulating viscous, compressible fluid flow about complex aerodynamic configurations. The technology solves the Reynolds-averaged Navier-Stokes equations using structured, overset computational grids. It includes the capability for simulating multiple moving bodies acting under prescribed or aerodynamically forced motion. OVERFLOW 2 is a merge of the previously developed OVERFLOW 1.8 and OVERFLOW-D codes.
Notes: Written in FORTRAN

Software Details

Category
Aeronautics
Reference Number
LAR-19668-1
Release Type
U.S. Release Only
Operating System
Linux
Contact Us About This Technology

Langley Research Center
Stay up to date, follow NASA's Technology Transfer Program on:
facebook twitter linkedin youtube
Facebook Logo Twitter Logo Linkedin Logo Youtube Logo