Parida, BK (1992) Recent advances in high temperature materials for aerospace applications and their fatigue life analysis methods. In: Proceedings of the International Symposium, 12-15 Dec 1992, Bangalore, India.Full text not available from this repository.
Recent advances in aerospace materials technology are reviewed with emphasis on high temperature engineered materials and various forms of composites. The fatigue-creep-environment interaction models that are currently used for fatigue crack growth analysis at high temperatures13; are briefly reviewed. A linear superposition model is presented which is capable of accurately predicting the fatigue crack growth rate of Ti-24Al-11Nb (alpha-2) at 649 C and Ti-1100 at 593 C.
|Item Type:||Conference or Workshop Item (Paper)|
|Uncontrolled Keywords:||Heat resistant alloys;Spacecraft construction materials; Fatigue life;Crack propagation;Titanium alloys;Carbon-carbon composites;Intermetallics;Creep properties|
|Subjects:||CHEMISTRY AND MATERIALS > Chemistry and Materials (General)|
|Division/Department:||Structural Integrity Division|
|Depositing User:||M/S ICAST NAL|
|Date Deposited:||31 Mar 2008|
|Last Modified:||24 May 2010 09:55|
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