Temperature-pressure-time relations in a closed cryogenic container
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Huntley, Sidney C↗
Engineering topics
Huntley, Sidney C
Publications and source records attributed to Huntley, Sidney C.
Effect of compressor-outlet air bleed on performance of a centrifugal-flow turbojet engine with a constant-area jet nozzle
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Huntley, Sidney C↗
Altitude-chamber Performance of British Roll-royce Nene II Engine IV : Effect of Operational Variables on Temperature Distribution at Combustion-chamber Outlets
Temperature surveys were made at the combustion-chamber outlets of a British Rolls-Royce Nene II engine. The highest mean nozzle-vane and mean gas temperatures were found to occur at a radius approximately 75% of the nozzle-vane length from the inner ring of the nozzle-vane assembly. Variations in engine speed, jet-nozzle area, simulated altitude, and simulated flight speed altered the temperature level but did not materially affect the pattern of radial temperature distribution.
COMBUSTION - TURBINE ENGINES↗
Theoretical evaluation of the ducted-fan turbojet engine
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ENGINES, TURBOJET - PERFORMANCE↗