TY  - RPRT
TI  - Liquid propellant rocket engine combustion simulation with a time-accurate CFD method
AU  - Chen, Y. S.
AU  - Shang, H. M.
AU  - Liaw, Paul
AU  - Hutt, J.
PY  - 1993
UR  - https://ntrs.nasa.gov/citations/19950017025
ID  - 19950017025
ER  -