Print Email Facebook Twitter High temperature gas turbine materials Title High temperature gas turbine materials Author Wanhill, R.J.H. Institution National Aerospace Laboratory NLR Date 1975-06-30 Abstract The requirements and problems of high temperature materials in gas turbines are reviewed, with specific reference to turbine discs, blades, vanes and combustion cans. The mechanical and environmental property requirements of these components are discussed, followed by an overview of the types of materials used. Lastly, there is a summary of the problems of creep and stress rupture, low cycle fatigue (including thermal fatigue), oxidation and hot corrosion. Subject CorrosionCreep propertiesCreep rupture strengthEngine partsFatigueGas turbinesHeat resistant alloysHigh temperature environmentsOxidationRequirementsStress cyclesThermal fatigue To reference this document use: http://resolver.tudelft.nl/uuid:4ee3b948-f49e-4794-a3f7-eb3be8b02d2d Publisher Nationaal Lucht- en Ruimtevaartlaboratorium Access restriction Campus only Source NLR-TR 75098 U Part of collection Aerospace Engineering Reports Document type report Rights (c)1975 National Aerospace Laboratory NLR Files PDF NLR_TR_75098_U.pdf 9.93 MB Close viewer /islandora/object/uuid:4ee3b948-f49e-4794-a3f7-eb3be8b02d2d/datastream/OBJ/view