TY  - RPRT
TI  - Development of an algebraic stress/two-layer model for calculating thrust chamber flow fields
AU  - Chen, C. P.
AU  - Shang, H. M.
AU  - Huang, J.
PY  - 1993
UR  - https://ntrs.nasa.gov/citations/19950017022
ID  - 19950017022
ER  -