TY  - RPRT
TI  - Numerical analysis of bipropellant combustion in liquid thrust chambers by an Eulerian-Eulerian approach
AU  - Dang, A. L.
AU  - Navaz, H. K.
AU  - Rangel, R. H.
PY  - 1992
UR  - https://ntrs.nasa.gov/citations/19920071515
ID  - 19920071515
ER  -