Stresses Due to Temperature Gradients in Ceramic-Matrix-Composite Aerospace Components-Reference-Cited by-同舟云学术

Stresses Due to Temperature Gradients in Ceramic-Matrix-Composite Aerospace Components

Published:2004-12-22 Issue:1 Volume:82 Page:161-168
ISSN:0002-7820
Container-title:Journal of the American Ceramic Society
language:en
Short-container-title:

Author:

John Reji,Zawada Larry P.,Kroupa Joseph L.

Publisher

Wiley

Subject

Materials Chemistry,Ceramics and Composites

Link

http://onlinelibrary.wiley.com/wol1/doi/10.1111/j.1151-2916.1999.tb01736.x/fullpdf

Reference29 articles.

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2. D. M. Dix J. S. Petty Aircraft Engine Technology Gets a Second Wind Aerospace Am. 36 39 1990

3. R. J. Hill The Challenge of Integrated High Performance Turbine Engine Technology (IHPTET) Proceedings of the 11th International Symposium on Air Breathing Engines F. S. Billig 1993

4. Ceramic Composite Turbine Engine Component Evaluation;Fohey;Ceram. Eng. Sci. Proc.,1995

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