2012
DOI: 10.1016/j.nucengdes.2011.11.019
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Numerical simulation of aircraft crash on nuclear containment structure

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Cited by 59 publications
(13 citation statements)
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“…It was explicit finite element method (FEM) using the commercial FEM tool, ABAQUS/Explicit. This method has been widely used for evaluation of crash or stamping with high speed dynamic material behavior [9][10][11] . Comparisons were made between the result of collision simulations by the FEM tool and their corresponding experimental result and then led to a good agreement in terms of energy absorption and postdeformation between them [9][10][11][12][13] .…”
Section: Application Of Finite Element Methodsmentioning
confidence: 99%
See 1 more Smart Citation
“…It was explicit finite element method (FEM) using the commercial FEM tool, ABAQUS/Explicit. This method has been widely used for evaluation of crash or stamping with high speed dynamic material behavior [9][10][11] . Comparisons were made between the result of collision simulations by the FEM tool and their corresponding experimental result and then led to a good agreement in terms of energy absorption and postdeformation between them [9][10][11][12][13] .…”
Section: Application Of Finite Element Methodsmentioning
confidence: 99%
“…The high velocity of the projectile rapidly deformed the impact area before its kinetic energy was propagated into the neighboring area. This is a characteristic of impact such as abrupt object collision [9][10][11][12][13] .…”
Section: Development Of a Finite Element Modelmentioning
confidence: 99%
“…The material properties are shown in Table 3. The impact is assumed to occur horizontally and is analyzed following an uncoupled procedure in which its effect onto the nuclear power plant is considered through the application of a short-time load (See References [2], [6], [8], [9] and [10]) as shown in Fig. 12.…”
Section: Aircraft Impact On Nuclear Power Plant (1964)mentioning
confidence: 99%
“…left: Model of the impact of a Boeing 747 into a fictious containment building(Arros, 2007); right: model of an RC containment and the damage after impact of a Phantom F4(Iqbal et al, 2012) Load-time function in case of impact of a Phantom F4 fighter with 215 m/s, (based onRiera (1968),Wolf (1978) andSugano et al (1993-1)) …”
mentioning
confidence: 99%