Engineering Data on New Aerospace Structural Materials

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Report Number: AFML TR 73-114
Author(s): Deel, O. L., Mindlin, H., Ruff, P. E.
Corporate Author(s): Battelle Columbus Laboratories
Date of Publication: 1973-06
Pages: 148
DoD Task:
Identifier: AD0762305

The major objectives of the research program were to evaluate newly developed materials of interest to the Air Force for potential structural airframe usage, and to provide data sheet type presentations of engineering data for these materials. The effort covered in the report has concentrated on X2048- T851 plate, 7050-T73651 plate, 21-6-9 annealed sheet, Ti-8Mo-8V-2Fe-3Al STA sheet, Ti-6Al-2Zr-2Sn-2Mo-2Cr STA plate, and Ti-6Al-6V-2Sn STA isothermal die forgings. The properties investigated include tension, compression, shear, bend, impact, fracture toughness, fatigue, creep and stress-rupture, and stress corrosion at selected temperatures.

Provenance: Lockheed Martin Missiles & Fire Control

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