Combined Analysis of Thruster Plume Behavior in Rarefied Region by Preconditioned Navier-Stokes and DSMC Methods
- 1 January 2009
- journal article
- Published by Japan Society for Aeronautical and Space Sciences in TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
- Vol. 52 (177), 135-143
- https://doi.org/10.2322/tjsass.52.135
Abstract
No abstract availableThis publication has 18 references indexed in Scilit:
- Plume impingement investigation using Monte-Carlo computationsProceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2006
- DSMC and Navier-Stokes Study of Backflow for Nozzle Plumes Expanding into VacuumAIP Conference Proceedings, 2005
- A Combined Continuum/DSMC Technique for Multiscale Analysis of Microfluidic FiltersJournal of Computational Physics, 2002
- PRECONDITIONING TECHNIQUES IN COMPUTATIONAL FLUID DYNAMICSAnnual Review of Fluid Mechanics, 1999
- Preconditioning applied to variable and constant density flowsAIAA Journal, 1995
- Low-density nozzle flow by the direct simulation Monte Carlo and continuum methodsJournal of Propulsion and Power, 1995
- Preconditioning applied to variable and constant density time-accurate flows on unstructured meshesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1994
- A Coupled Implicit Method for Chemical Non-equilibrium Flows at All SpeedsJournal of Computational Physics, 1993
- Modeling of a small hydrazine thruster plume in the transition flow regimeJournal of Propulsion and Power, 1990
- A numerical method for solving incompressible viscous flow problemsJournal of Computational Physics, 1967