TY  - RPRT
TI  - A three-dimensional incompressible flow simulation method and its application to the Space Shuttle main engine. II Turbulent flow
AU  - Chang, J. L. C.
AU  - Rosen, R.
AU  - Dao, S. C.
AU  - Kwak, D.
PY  - 1985
UR  - https://ntrs.nasa.gov/citations/19850060949
ID  - 19850060949
ER  -