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Advanced materials and fabrication processes for supersonic cruise aircraftResearch and development programs to develop high-strength aluminum alloys and low-cost materials and fabrication techniques for titanium alloys are being conducted. Thirteen aluminum alloy compositions are being evaluated. A section of a production component was fabricated using superplastic forming and diffusion bonding (SPF/DB) and fabrication studies are being conducted on three low temperature forming beta titanium alloys. Cost studies indicate substantial structural cost reduction potentials resulting from the use of both aluminum alloys and low-cost titanium fabrication techniques. Lowest overall costs are indicated for a composite/aluminum or composite titanium structure.
Document ID
19810009488
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Guess, M. K.
(Lockheed-California Co. Burbank, CA, United States)
Kaneko, R. S.
(Lockheed-California Co. Burbank, CA, United States)
Wald, G. G.
(Lockheed-California Co. Burbank, CA, United States)
Date Acquired
August 11, 2013
Publication Date
March 1, 1981
Publication Information
Publication: NASA. Langley Research Center Supersonic Cruise Res., 1979, Pt. 2
Subject Category
Metallic Materials
Accession Number
81N18011
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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