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  2. 5052 aluminium alloy - Wikipedia

    en.wikipedia.org/wiki/5052_aluminium_alloy

    5052 is an aluminium–magnesium alloy, primarily alloyed with magnesium and chromium. 5052 is not a heat treatable aluminum alloy, but can be hardened through cold working. [ 2 ] Chemical properties

  3. Aluminium alloy - Wikipedia

    en.wikipedia.org/wiki/Aluminium_alloy

    Note that the term aircraft aluminium or aerospace aluminium usually refers to 7075. [65] [66] 4047 aluminium is a unique alloy used in both the aerospace and automotive applications as a cladding alloy or filler material. As filler, aluminium alloy 4047 strips can be combined to intricate applications to bond two metals. [67]

  4. Aluminium–magnesium alloys - Wikipedia

    en.wikipedia.org/wiki/Aluminium–magnesium_alloys

    At 70 °C, they form after 3 months, at 100 °C after 3 days and at 150 °C after one to nine hours. If further time passes at elevated temperature, the plaques grow together to form a contiguous film. This has a negative effect on corrosion resistance, but can be dissolved by heat treatment.

  5. Precipitation hardening - Wikipedia

    en.wikipedia.org/wiki/Precipitation_hardening

    Precipitation hardening, also called age hardening or particle hardening, is a heat treatment technique used to increase the yield strength of malleable materials, including most structural alloys of aluminium, magnesium, nickel, titanium, and some steels, stainless steels, and duplex stainless steel.

  6. Table of specific heat capacities - Wikipedia

    en.wikipedia.org/wiki/Table_of_specific_heat...

    Table of specific heat capacities at 25 °C (298 K) unless otherwise noted. [citation needed] Notable minima and maxima are shown in maroon. Substance Phase Isobaric mass heat capacity c P J⋅g −1 ⋅K −1 Molar heat capacity, C P,m and C V,m J⋅mol −1 ⋅K −1 Isobaric volumetric heat capacity C P,v J⋅cm −3 ⋅K −1 Isochoric ...

  7. Hiduminium - Wikipedia

    en.wikipedia.org/wiki/Hiduminium

    R.R.58, also known as Aluminium 2618, comprising 2.5 copper, 1.5 magnesium, 1.0 iron, 1.2 nickel, 0.2 silicon, 0.1 titanium and the remainder aluminium, and originally intended for jet engine compressor blades, was used as the main structural material for the Concorde airframe, supplied by High Duty Alloys, it was also known as AU2GN to the ...

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  9. Heat treating - Wikipedia

    en.wikipedia.org/wiki/Heat_treating

    Heat treating furnace at 1,800 °F (980 °C) Heat treating (or heat treatment) is a group of industrial, thermal and metalworking processes used to alter the physical, and sometimes chemical, properties of a material. The most common application is metallurgical.

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