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Titanium/beryllium laminates : Fabrication, mechanical properties, and potential aerospace applications

Author
Chamis, C. C.
Published
May 1, 1978.
Physical Description
1 electronic document
Additional Creators
Lark, R. F.
Online Version

Availability

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
The investigation indicated that structural laminates can be made which have: a modulus of elasticity comparable to steel, fracture strength of comparable to the yield strength of titanium, density comparable to aluminum, impact resistance comparable to titanium, and little or no notch sensitivity. These laminates can have stiffness and weight advantages over other materials including advanced fiber composites, in some aerospace applications where buckling resistance, vibration frequencies, and weight considerations control the design.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19780013278.
Accession ID: 78N21221.
E-9508.
NASA-TM-73891.
Natl. SAMPE Symp. and Exhibition; 2-4 May 1978; Anaheim, CA; United States.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15729256