NASA STI Repository (National Aeronautics and Space Administration) · 1983 · 11 citations · 0 references
Open access
EngineeringMechanical EngineeringEnergy SystemsInternal Combustion EnginesPerformance-based DesignEngine Cooling SystemsEngine DesignEngine EfficiencyEngine PerformanceEngine Performance CharacteristicsEngine SystemsOff-design PerformanceRig DesignSecondary Flow EffectsTurbine CoolingTurbine DesignTurbine EfficiencyTurbine PerformanceTurbine Technology
A rig test of the cooled high-pressure turbine component for the Energy Efficient Engine was successfully completed. The principal objective of this test was to substantiate the turbine design point performance as well as determine off-design performance with the interaction of the secondary flow system. The measured efficiency of the cooled turbine component was 88.5 percent, which surpassed the rig design goal of 86.5 percent. The secondary flow system in the turbine performed according to the design intent. Characterization studies showed that secondary flow system performance is insensitive to flow and pressure variations. Overall, this test has demonstrated that a highly-loaded, transonic, single-stage turbine can achieve a high level of operating efficiency.