Thermal barrier coated Nextel 720 fiber/mullite matrix composites: their potential for long-term high temperature use in gas turbines

Ceramic Engineering and Science Proceedings

Volumn 21, Issue 3, 2000, Pages 613-618

  Goering, J ^a   Kanka, B ^a   Steinhauser, U ^a   Schneider, H ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

CRACK PROPAGATION; CREEP; FIBER REINFORCED MATERIALS; GAS TURBINES; HIGH TEMPERATURE OPERATIONS; PHASE COMPOSITION; STRENGTH OF MATERIALS; TENSILE TESTING;

ALUMINA SILICATE FIBERS; CONTINUOUS OXIDE FIBER; HIGH POROUS MULLITE MATRICES; MECHANICAL STABILITY; OXIDE MATRIX COMPOSITES; THERMAL PROTECTION SYSTEMS;

CERAMIC MATRIX COMPOSITES;

EID: 0033667028     PISSN: 01966219     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (14)