A Heat Transfer Investigation of Ejector Systems with 90 Deg Turns. NERVA Program
Heat transfer characteristics of ejector systems for turning rocket exhaust gases through 90 deg
Mandell, B.↗
Engineering topics
Mc Farland, B. L.
Publications and source records attributed to Mc Farland, B. L..
SCALE MODEL TESTING OF 90 DEG TURN EJECTOR SYSTEMS FOR ROCKET ENGINE ALTITUDE SIMULATION
Scale model testing of 90 degree turn ejector systems for rocket engine altitude simulation
NUCLEAR ROCKET↗
SCALE MODEL TESTING OF 90 DEG TURN EJECTOR SYSTEMS FOR ROCKET ENGINE ALTITUDE SIMULATION
Scale model testing of 90-deg turn ejector systems for rocket engine simulation
ROCKET ENGINE↗