Fracture Toughness Analysis of Metastable Beta Titanium Alloys
Department of Defense
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Accurate Automation Corp
7001 Shallowford Road, Chattanooga, TN, 37421
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AbstractThe feasibility of fabricating hypersonic aircraft components from metastable Beta Titanium alloy (Beta 21S) will be investigated. Techniques for the fabrication of the leading edges, inlet, and nozzle areas of a hypersonic (Mach 4-5) testbed aircraft from Beta 21S will be selected and preliminary drawings, specifications, and test procedures for these components will be developed.
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