Principal Research Results Development of the Temperature Prediction Method for Hot Gas Path Parts of 1300 ℃ Class Gas Turbines Background Electric power companies are working to extend the remaining life of gas turbi - Hot working - Document - PDFSEARCH.IO

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	Principal Research Results Development of the Temperature Prediction Method for Hot Gas Path Parts of 1300 ℃ Class Gas Turbines Background Electric power companies are working to extend the remaining life of gas turbi Add to Reading List Document Date: 2008-09-29 03:15:21 Open Document File Size: 225,36 KB Share Result on Facebook City Amsterdam / Vienna / / Country Japan / Austria / United States / Netherlands / / Facility Combustor Inlet Film Cooling Air port Ratio / / IndustryTerm gas turbine / hot gas path parts / class gas turbine / / NaturalFeature Combustor Inlet / / Organization Energy Engineering Research Laboratory / / Person Masahiko Morinaga / Toshihiko Takahashi / / Position Research Scientist / Thermal Engineering Sector / Research Scientist / Advanced Power Engineering Sector / / ProvinceOrState Hawaii / / Technology Fluid Dynamics / heat transfer / Simulation / / SocialTag Heat transfer Physical quantities Jet engines Heat conduction Thermodynamics Thermal barrier coating Combustor Gas turbine Turbine Chemistry

Principal Research Results Development of the Temperature Prediction Method for Hot Gas Path Parts of 1300 ℃ Class Gas Turbines Background Electric power companies are working to extend the remaining life of gas turbiAdd to Reading List