Fracture Toughness Analysis of Metastable Beta Titanium Alloys
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7001 Shallowford Road, Chattanooga, TN, 37421
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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