Effects of frequency on fatigue behavior of CVI C/SiC at elevated temperature

Author:

Mall Shankar,Engesser John Mark

Publisher

Elsevier BV

Subject

General Engineering,Ceramics and Composites

Reference18 articles.

1. Applications of CMCs to turbojet engines: overview of the SEP experience;Spriet;Key Eng Mater,1997

2. Effinger MR, Koening JR, Halbig MC. C/SiC mechanical and thermal design data for a turbopump blisk. In: Proceedings of the 21st annual conference on composites, materials and structures, Cocoa Beach, FL, January 26–31; 1997. p. 273–289.

3. Ceramics matrix composites for rocket engine turbine applications;Herball;Trans ASME,1993

4. Herball TP, Eckel AJ. Ceramics composites portend long turbopump lives. In: SAE aerospace atlantic conference and exposition, Dayton, OH, April 20–23; 1993.

5. Characterization of damage accumulation in a carbon fiber-reinforced silicon carbide ceramic matrix composite (C/SiC) subjected to mechanical loadings at intermediate temperature;Verilli,2000

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