TY  - RPRT
TI  - Method for Determining Optimum Division of Power Between Jet and Propeller for Maximum Thrust Power of a Turbine-propeller Engine
AU  - Trout, Arthur M
AU  - Hall, Eldon W
PY  - 1950
UR  - https://ntrs.nasa.gov/citations/19930082829
ID  - 19930082829
ER  -