NASA NTRS · 20180004682
High Temperature Ceramic Microstructure and Interface Evolution during Exposure to Particulate Laden Combustion Flows in Gas Turbine Engines
Abstract
Objective: To innovate sandphobic coating and surface modification for high temperature turbine blades to resist sand glaze build-up and related Calcia-Magnesia-Alumina-Silicate (CMAS) attack on Thermal/Environmental Barrier Coatings (T/EBCs).
Explore related subjects
Keep this discovery
Explore connections, maps & timelines
Nieto, Andy, Walock, Michael, Ghoshal, Anindya, Murugan, Muthuvel, Bravo, Luis, Barnett, Blake, Pepi, Marc, Swab, Jeff, Gamble, William, Graybeal, Mark, Zhu, Dongming, Wright, Andrew, Luo, Jian, Rowe, Chris, Pegg, Robert, Kerner, Kevin. 2018-01-25. High Temperature Ceramic Microstructure and Interface Evolution during Exposure to Particulate Laden Combustion Flows in Gas Turbine Engines. https://ntrs.nasa.gov/citations/20180004682
Cite the original work for its findings. Save a collection to share your selection of sources.