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  2. 7075 aluminium alloy - Wikipedia

    en.wikipedia.org/wiki/7075_aluminium_alloy

    It is produced in many tempers, some of which are 7075-0, 7075-T6, 7075-T651. The first 7075 was developed in secret by a Japanese company, Sumitomo Metal, in 1935, [3] but reverse engineered by Alcoa in 1943, after examining a captured Japanese aircraft. [4] 7075 was standardized for aerospace use in 1945.

  3. File:Thermal expansion of aluminum and some aluminum alloys ...

    en.wikipedia.org/wiki/File:Thermal_expansion_of...

    Short title: Thermal expansion of aluminum and some aluminum alloys: Author: Hidnert, P.; Krider, H.S. Software used: Adobe Acrobat 9.0: Conversion program

  4. Densities of the elements (data page) - Wikipedia

    en.wikipedia.org/wiki/Densities_of_the_elements...

    New York: The International Nickel Company, Inc., 1941: 16. — "Values ranging from 21.3 to 21.5 gm/cm 3 at 20 °C have been reported for the density of annealed platinum; the best value being about 21.45 gm/cm 3 at 20 °C." 21.46 g/cm 3 — Rose, T. Kirke. The Precious Metals, Comprising Gold, Silver and Platinum. New York: D. Van Nostrand ...

  5. 7075-T6 aluminium - Wikipedia

    en.wikipedia.org/?title=7075-T6_aluminium&...

    7075-T6 aluminium. Add languages. Add links. ... Upload file; Special pages; ... Get shortened URL; Download QR code; Print/export Download as PDF; Printable version ...

  6. Template:Aluminium alloys - Wikipedia

    en.wikipedia.org/wiki/Template:Aluminium_alloys

    Template: Aluminium alloys. Add languages ... Upload file; Special pages; Permanent link; Page information; Get shortened URL; Download QR code; Print/export Download ...

  7. 7068 aluminium alloy - Wikipedia

    en.wikipedia.org/wiki/7068_aluminium_alloy

    7068 alloy is a 7000 series aluminium-zinc alloy registered with the US Aluminium Association and produced to AMS 4331 (chemical composition and mechanical properties) and AMS 2772 (heat treatment). 7068 alloy ‘A’ and ‘B’ tensile data and fatigue properties have been ratified for inclusion in MIL Handbook 5 / MMPDS.

  8. Magnalium - Wikipedia

    en.wikipedia.org/wiki/Magnalium

    Alloys with small amounts of magnesium (about 5%) exhibit greater strength, greater corrosion resistance, and lower density than pure aluminium. Such alloys are also more workable and easier to weld than pure aluminum. [1] Alloys with high amounts of magnesium (around 50%) are brittle and more susceptible to corrosion than aluminum.

  9. 7065 aluminium alloy - Wikipedia

    en.wikipedia.org/wiki/7065_aluminium_alloy

    The combination of high strength and fracture toughness properties and corrosion resistance makes 7065 suitable as a replacement for 7010, 7050, 7075, 7475 and other alloys for critical intermediate thickness applications. [3] Spar, rib, and integrally machined structural parts for new, derivative, or retrofit aircraft. [3]

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