Title of article
Numerical simulations of target hole diameters for hypervelocity impacts into elevated and room temperature bumpers
Author/Authors
B.M. Corbett، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2006
Pages
10
From page
431
To page
440
Abstract
Normal impacts between 3.175 mm diameter 1100-O Al spherical projectiles and 1.6 mm thick 6061-T6 Al targets are considered for both room temperature and heated targets. The elevated target temperatures under examination are 110 and 210 °C, and the simulated impact velocities range from approximately 2 to7 km/s. The AUTODYN v.5 hydrocode is used to generate data that are compared to empirical data obtained from the literature, and to that obtained with the University of Denver Research Instituteʹs (DRI) two-stage light gas gun. The effect of using applicable strength and fracture models currently available in AUTODYN to replicate both room and elevated temperature target hole diameters is also examined. It was found that the numerical simulations for both room and elevated temperature targets predict hole diameters that differ approximately 0.1–13% from the DRI empirical data.
Keywords
Temperature Effects , hypervelocity impact , Hole diameter , Numerical simulation , orbital debris
Journal title
International Journal of Impact Engineering
Serial Year
2006
Journal title
International Journal of Impact Engineering
Record number
1250995
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