TY  - RPRT
TI  - Core compressor exit stage study. 1: Aerodynamic and mechanical design
AU  - Burdsall, E. A.
AU  - Canal, E., Jr.
AU  - Lyons, K. A.
PY  - 1979
UR  - https://ntrs.nasa.gov/citations/19800010836
ID  - 19800010836
ER  -