TY  - RPRT
TI  - Modeling of supersonic combustor flows using parallel computing
AU  - Riggins, D.
AU  - Underwood, M.
AU  - Mcmillin, B.
AU  - Reeves, L.
AU  - Lu, E. J.-L.
PY  - 1992
UR  - https://ntrs.nasa.gov/citations/19930036723
ID  - 19930036723
ER  -