AZ61A

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The damage model parameters for Magnesium AZ61A alloy were fitted using DMGfit_55p_v1p1. The original sources, the fitting procedure and results are detailed below.

Contents

Source Data

The source data was based on the digitization of AZ61A stress-strain curves. A compression and a tension stress-strain curves, respectively, were digitized.

Mg.009 AZ61A magnesium alloy forging compressive stress-strain curve. [1]

Composition: Mg-6Al-1Zn. UNS M11610
Mg.009 AZ61A magnesium alloy forging tensile stress-strain curve. [1]

Composition: Mg-6Al-1Zn. UNS M11610



For the source we digitized Mg stress-strain curves.

Digitized data:


Fitting Procedure

Explain the fitting procedure and rationalization


Results

caption goes here


References

  1. 1.0 1.1 "Magnesium Design", Dow Chemical Co., 1957. As published in Aerospace Structural Metals Handbook, vol 3, Code 3603, CINDAS/USAF CRDA Handbooks Operation, Purdue University, 1995, p4
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