Design issues in using integral textile ceramic composites in turbine engine combustors

Journal of Propulsion and Power

Volumn 21, Issue 2, 2005, Pages 314-326

  Cox, B N ^a,b   Yang, Q D ^a,c   Marshall, D B ^a,b   Davis, J B ^a,c  

^a ROCKWELL SCIENTIFIC COMPANY   (United States)

^b Dept of Transportation   (United States)

^c Composite Materials Department ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ASYMPTOTIC STABILITY; CERAMIC MATERIALS; COMBUSTION; COMBUSTORS; COOLING; HEAT TRANSFER; STRESS ANALYSIS; SURFACE PROPERTIES; TEXTILES; THERMAL CONDUCTIVITY; THERMAL EXPANSION; TURBINES;

CERAMIC COMPOSITES; HOT-STRUCTURE; THERMAL MISMATCH; TURBINE ENGINE COMBUSTORS;

COMPOSITE STRUCTURES;

EID: 15944417157     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/1.11010     Document Type: Article

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