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Currently viewing the tag: "turbine cooling"

Jet Engine Design: Turbine Cooling

On May 1, 2013 · In Aerodynamics, Technology

As I described in a previous post, the efficiency of the gas turbine cycle increases as the turbine entry temperature (TET) is increased. Therefore the hotter the combustion gases that enter the first turbine stage the more specific power the jet engine can produce. Of course the TET is […]

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