3D THERMO-MECHANICAL MODELING OF MULTILAYERED TBC S FOR GAS TURBINE ENGINES
Abstract
The proposed research here integrates material selection and process design capabilities (to deposit coatings of different controlled microstructures) with computer based simulation of these systems to provide a comprehensive and theoretically based understanding of stresses, strain energies, and temperature gradients that drive coating failure.
Document Details
- Document Type
- DoD Grant Award
- Publication Date
- Aug 12, 2021
- Source ID
- FA95502010075
Entities
People
- Alfredo Valarezo
Organizations
- Air Force Office of Scientific Research
- United States Air Force
- Universidad San Francisco de Quito