TY  - RPRT
TI  - High performance Solid Rocket Motor (SRM) submerged nozzle/combustion cavity flowfield assessment
AU  - Freeman, J. A.
AU  - Chan, J. S.
AU  - Murph, J. E.
AU  - Xiques, K. E.
PY  - 1987
UR  - https://ntrs.nasa.gov/citations/19880009238
ID  - 19880009238
ER  -