共 50 条
- [31] COMPOSITIONALLY GRADED THERMAL BARRIER COATINGS FOR HIGH-TEMPERATURE AERO GAS-TURBINE COMPONENTS SURFACE & COATINGS TECHNOLOGY, 1992, 54 (1-3): : 58 - 63
- [32] HIGH-TEMPERATURE EROSION RESISTANCE OF COATINGS FOR USE IN GAS-TURBINE ENGINES SURFACE & COATINGS TECHNOLOGY, 1992, 52 (01): : 65 - 79
- [34] DEVELOPMENT OF NONDESTRUCTIVE TESTING METHOD FOR EXAMINING THERMAL RESISTANCE OF THERMAL BARRIER COATINGS ON GAS TURBINE BLADES PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2013, VOL 4, 2013,
- [36] Multilayer Thermal Barrier Coatings for Gasified Coal Based Turbine Engines ADVANCED MATERIALS & PROCESSES, 2013, 171 (05): : 49 - 51
- [37] Development of NiCrAlY alloys for corrosion-resistant coatings and thermal barrier coatings of gas turbine components JOURNAL OF PRESSURE VESSEL TECHNOLOGY-TRANSACTIONS OF THE ASME, 1999, 121 (04): : 384 - 387
- [38] EFFECT OF COATINGS BARRIER PROPERTIES ON CORROSION-RESISTANCE ABSTRACTS OF PAPERS OF THE AMERICAN CHEMICAL SOCIETY, 1988, 195 : 30 - PMSE
- [39] CORROSION-RESISTANCE OF GAS-THERMAL ALUMINUM AND ZINC COATINGS UNDER OPERATING-CONDITIONS PROTECTION OF METALS, 1990, 26 (03): : 356 - 358
- [40] Governing Parameters Influencing CMAS Adhesion and Infiltration into Environmental/Thermal Barrier Coatings in Gas Turbine Engines PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2019, VOL 6, 2019,