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This paper extends the gradient-driven interface degradation framework to thermal barrier coating (TBC) spallation on aero-engine turbine blades. It argues that TBC spallation and liquid rocket engine combustion chamber layered spallation share the same physical mechanism—vacancy thermomigration-driven interface condensation coupled with modal locking.
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Internal reference: SFM-2026-033. Version 1.4.0 (May 2026). Key changes in v1.4.0: the Cantor function and Peano curve are anchored directly to Cantor (1883), Peano (1890), and Sagan (1994) as classical mathematical references. The honest boundaries section now states that these classical mathematical constructs belong to the public domain and are ...
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International Journal of Applied Earth Observation and Geoinformation, 2018
Luis A. Méndez-Barroso +1 more
exaly
Luis A. Méndez-Barroso +1 more
exaly
Local Elastic Properties of Cells Studied by SFM
Applied Surface Science, 1999Janusz Lekki +2 more
exaly

