Nozzle Turbine at Jasper Biddell blog

Nozzle Turbine. The nozzle serves to convert any energy remaining in the flow (after the turbine) to kinetic energy by decreasing pressure and accelerating. Turbofan engines sometimes employ a coannular nozzle where the core flow exits the center nozzle while the fan flow exits the annular nozzle. The nozzle performance equations work just as well for rocket engines except that rocket nozzles always expand the flow to some supersonic exit velocity. All gas turbine engines have a nozzle to produce thrust, to conduct the exhaust gases back to the free stream, and to set the mass flow rate through the engine.

Impulse turbine,Nozzle turbine,Turbine
from www.eternoohydro.com

Turbofan engines sometimes employ a coannular nozzle where the core flow exits the center nozzle while the fan flow exits the annular nozzle. The nozzle performance equations work just as well for rocket engines except that rocket nozzles always expand the flow to some supersonic exit velocity. All gas turbine engines have a nozzle to produce thrust, to conduct the exhaust gases back to the free stream, and to set the mass flow rate through the engine. The nozzle serves to convert any energy remaining in the flow (after the turbine) to kinetic energy by decreasing pressure and accelerating.

Impulse turbine,Nozzle turbine,Turbine

Nozzle Turbine Turbofan engines sometimes employ a coannular nozzle where the core flow exits the center nozzle while the fan flow exits the annular nozzle. Turbofan engines sometimes employ a coannular nozzle where the core flow exits the center nozzle while the fan flow exits the annular nozzle. The nozzle serves to convert any energy remaining in the flow (after the turbine) to kinetic energy by decreasing pressure and accelerating. All gas turbine engines have a nozzle to produce thrust, to conduct the exhaust gases back to the free stream, and to set the mass flow rate through the engine. The nozzle performance equations work just as well for rocket engines except that rocket nozzles always expand the flow to some supersonic exit velocity.

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