Analysis of large solid propellant rocket engine exhaust plumes using the direct simulation Monte Carlo method

Publisher Website

9 January 1984

proceedings article
Published by American Institute of Aeronautics and Astronautics (AIAA)

https://doi.org/10.2514/6.1984-496

Abstract

No abstract available

This publication has 1 reference indexed in Scilit:

Breakdown of translational and rotational equilibrium in gaseous expansions
AIAA Journal, 1970