Performance of a 10 deg conical plug nozzle using a turbojet gas generator
Internal performance data for conical plug nozzle of turbojet gas engine
Huntley, S. C.↗
Engineering topics
Huntley, S. C.
Publications and source records attributed to Huntley, S. C..
Thrust and pumping characteristics of cylindrical ejectors using afterburning turbojet gas generator
Static tests of cylindrical ejectors having ejector to primary diameter ratios from 1.1 to 1.6 and ejector length to primary nozzle diameter ratios from 0.9 to 2.1 are reported. Power setting of the J85-13 turbojet engine was varied from part power to maximum afterburning. Corrected secondary weight flow ratio was varied from 0.02 to 0.08 over a range of exhaust nozzle pressure ratios from 2.0 to 9.0. Secondary flow temperature rise and pressure drop characteristics through the nacelle secondary flow passage were also obtained.
Samanich, N. E.↗
Propellant flow system components
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Hartmann, M. J.↗
Simulated nuclear heating of liquid hydrogen in a propellant tank
Simulated nuclear heating of liquid hydrogen in propellant tank
LIQUID HYDROGEN↗
Wall and bottom heating of liquid hydrogen in a propellant tank
Liquid hydrogen behavior during propellant tank wall and bottom heating
WALL TEMPERATURE↗
Propellant Heating Studies with Wall and Nuclear Heating
Propellant heating studies with wall and nuclear heating
NUCLEAR HEAT↗
COMBINED COMPRESSOR COOLANT INJECTION AND AFTERBURNING FOR TURBOJET THRUST AUGMENTATION
Combined compressor coolant injection and afterburning for turbojet engine thrust augmentation
AFTERBURNING↗