2015
DOI: 10.1016/j.msea.2015.05.007
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Drop weight impact behavior of functionally graded aluminum foam consisting of A1050 and A6061 aluminum alloys

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Cited by 48 publications
(27 citation statements)
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“…8 and 9 indicate the initial boundary between the two foam layers in the A6061/A1050 and ADC12/A1050 FG Al foam specimens. The deformation states for all the uniform Al foam specimens and FG Al foam specimens were similar to those in previously reported impact tests (Hangai et al, 2015) and static compression tests (Utsunomiya et al, 2010b. That is, the FG Al foam specimen first started to deform only in the weaker Al (A1050) foam layer and then deformed in the high-strength Al (A6061 or ADC12) foam layer.…”
Section: Fracture States Of Specimenssupporting
confidence: 83%
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“…8 and 9 indicate the initial boundary between the two foam layers in the A6061/A1050 and ADC12/A1050 FG Al foam specimens. The deformation states for all the uniform Al foam specimens and FG Al foam specimens were similar to those in previously reported impact tests (Hangai et al, 2015) and static compression tests (Utsunomiya et al, 2010b. That is, the FG Al foam specimen first started to deform only in the weaker Al (A1050) foam layer and then deformed in the high-strength Al (A6061 or ADC12) foam layer.…”
Section: Fracture States Of Specimenssupporting
confidence: 83%
“…The simple estimation method for the plateau stress was applied to estimate the plateau stresses for the uniform Al foams and each layer of the FG Al foams. Similar uniform and FG Al foams to those fabricated in this study have already been fabricated in previous studies , Hangai et al, 2015; therefore, the results obtained in the previous studies are also contained in the estimation carried out in this study. Through the comparison of the compression test results with the estimated results, the possibility of estimating plateau stresses by the simple estimation method is discussed for the uniform Al foams and each layer of the FG Al foams.…”
Section: Plateau Stress Estimation Of Impact Compression Test On Alumsupporting
confidence: 75%
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