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NASA NTRS ยท 19880057516

Elevated temperature durability of ceramic materials

Abstract

Fast fracture, stress rupture, and cyclic high temperature durability characterizations have been conducted for advanced silicon carbide and silicon nitride ceramics applicable to gas turbine hot section components. The fast fracture and stress rupture tests were conducted in four-point flexure at temperatures of up to 1540 C; the durability tests involved cycling specimens to temperatures of 1370 C and air quenching at 200 C for up to 3500 hrs. Materials with further reliability improvements are noted to be required for gas turbine hot section component applications.

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BibTeXRIS

Lindberg, Laura J.. 1988-07-01. Elevated temperature durability of ceramic materials. https://ntrs.nasa.gov/citations/19880057516

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