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Supplier: ASTM International
Description: test at 200°C under abrupt changes of stress states performed on a thin-walled tube specimen made of 2618 aluminum alloy.Show More
Supplier: RAF Electronic Hardware
Description: 5/16 Sq X 1-9/16 Length
- Type & Shape: Standoff
- Outside Diameter / Width: 0.3125 inch
- Body Length / Working Height: 1.56 inch
- Material: Aluminum
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Enhancement of Aluminum Alloy Forgings through Rapid Billet Heating
Studies were conducted to study the effects of rapid heating on the microstructure and mechanical properties in 2618 aluminum alloy forgings.
Influence of Various Parameters on the Determination of the Fatigue Crack Arrest Threshold
2618 Aluminum Alloy: Initial AK ~ 11 MPaVm(~A:,e/2) .
INFLUENCE OF VARIOUS PARAMETERS ON THE DETERMINATION OF THE FATIGUE CRACK ARREST THRESHOLD Members of the Fatigue Commission of the French Metallurgical Societ...
Abstract —This report presents the results of a round robin study on the fatigue crack arrest threshold (δKth) of 2618 aluminium alloy and AISI 316 steel.
on 2618 aluminum using the CGDS method for improved wear and corrosion resistance in marine applications such as aircraft catapult systems.
Development of viscoplastic constitutive equation through biaxial material testing
Ding, J.L. and Findley, W.N., "'48 Hour Multiaxial Creep and Creep Recovery of 2618 Aluminum Alloy at 200~ "" ASME J. AppL Mech., 51, 125-132(1984).
Elevated temperature endurance and creep properties of extruded 2D70 Al alloy rods
Nový et al.  investigated microstructure changes in 2618 aluminum alloy during aging and creep at 270°C at a constant load of 140 MPa, showing that fine and coherent precipitates of S phase distributed dispersively in the matrix of the alloy after …