TY  - RPRT
TI  - 3-D thermal analysis using finite difference technique with finite element model for improved design of components of rocket engine turbomachines for Space Shuttle Main Engine SSME
AU  - Sohn, Kiho D.
AU  - Ip, Shek-Se P.
PY  - 1988
UR  - https://ntrs.nasa.gov/citations/19880060807
ID  - 19880060807
ER  -