This paper describes a concurrent implementation of the Aerospace Launch System Implicit/Explicit Navier-Stokes code (ALSINS). This general code is the primary tool used by The Aerospace Corporation for comlex multi-body launch vehicle configurations and nozzle flow calculations. The code utilizes a finite volume TVD scheme for computing both steady state and unsteady solutions to the 3-D compressible Navier-Stokes equations.
A concurrent Navier-Stokes solver for implicit multibody calculations
Ein paralleles Navier-Stokes-Lösungsverfahren für impliziete Mehrkörperberechnungen
1995
11 Seiten, 4 Bilder, 10 Quellen
Conference paper
English
Launch-Vehicle Simulations Using a Concurrent, Implicit Navier-Stokes Solver
Online Contents | 1996
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