TY  - RPRT
TI  - Analysis of large solid propellant rocket engine exhaust plumes using the direct simulation Monte Carlo method
AU  - Hueser, J. E.
AU  - Brock, F. J.
AU  - Melfi, L. T., Jr.
AU  - Bird, G. A.
PY  - 1984
UR  - https://ntrs.nasa.gov/citations/19840035342
ID  - 19840035342
ER  -