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  2. Fatigue limit - Wikipedia

    en.wikipedia.org/wiki/Fatigue_limit

    For iron, aluminium, and copper alloys, is typically 0.4 times the ultimate tensile strength. Maximum typical values for irons are 170 MPa (24 ksi), aluminums 130 MPa (19 ksi), and coppers 97 MPa (14 ksi). [ 2 ]

  3. Fatigue (material) - Wikipedia

    en.wikipedia.org/wiki/Fatigue_(material)

    S-N curve for a brittle aluminium with an ultimate tensile strength of 320 MPa Materials fatigue performance is commonly characterized by an S-N curve , also known as a Wöhler curve . This is often plotted with the cyclic stress ( S ) against the cycles to failure ( N ) on a logarithmic scale . [ 31 ]

  4. 7075 aluminium alloy - Wikipedia

    en.wikipedia.org/wiki/7075_aluminium_alloy

    7075 aluminium alloy (AA7075) is an aluminium alloy with zinc as the primary alloying element. It has excellent mechanical properties and exhibits good ductility, high strength, toughness, and good resistance to fatigue.

  5. Aluminium alloy - Wikipedia

    en.wikipedia.org/wiki/Aluminium_alloy

    An important structural limitation of aluminium alloys is their lower fatigue strength compared to steel. In controlled laboratory conditions, steels display a fatigue limit, which is the stress amplitude below which no failures occur – the metal does not continue to weaken with extended stress cycles. Aluminium alloys do not have this lower ...

  6. 7050 aluminium alloy - Wikipedia

    en.wikipedia.org/wiki/7050_aluminium_alloy

    Aluminium 7050 alloy is a heat treatable alloy. It has high toughness, high strength. ... Fatigue strength 240 MPa Elastic modulus 70-80 GPa Poisson's ratio 0.33 ...

  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. 6061 aluminium alloy - Wikipedia

    en.wikipedia.org/wiki/6061_aluminium_alloy

    Most strength is recovered in the first few days to a few weeks. Nevertheless, the Aluminum Design Manual (Aluminum Association) recommends the design strength of the material adjacent to the weld to be taken as 165 MPa/24000 PSI without proper heat treatment after the welding. Typical filler material is 4043 or 5356.

  9. 1200 aluminium alloy - Wikipedia

    en.wikipedia.org/wiki/1200_aluminium_alloy

    1200 Aluminium alloy has aluminium as the major element, and has silicon, ... Fatigue strength: 49 MPa U.T.S. 130 MPa Yield strength: 100 MPa Latent Heat of Fusion: