A model for predicting the damage and oxidation dependent life of SCS-6/Ti-B21S [0]4 metal matrix composite /

482[] C and 650[] C. The material was also oxidized at 700 C and

Bibliographic Details

Main Author:	Foulk, James Wesley
Format:	Thesis eBook
Language:	English
Published:	[Place of publication not identified] : [publisher not identified] ; 1997.
Subjects:	Major aerospace engineering.
Online Access:	Link to OAKTrust copy