TY - GEN
T1 - Numerical simulation of complex damage behaviour of advanced aerospace structures subject to hypervelocity impact
AU - Rathnasabapathy, Minoo
AU - Litchfield, Andrew
AU - Bayandor, Javid
PY - 2009
Y1 - 2009
N2 - Numerical investigations into the complexities of hypervelocity impacts onto advanced aerospace structures provide an accurate description of the damage evolution and propagation through impacted structures. The accurate prediction of the dynamic behaviour and damage response upon hypervelocity impacts in microgravity enable an in-depth understanding of damage patterns in partially and fully damaged space structures. Numerical simulations using explicit finite elements codes were conducted to demonstrate the ability of Smoothed Particle Hydrodynamics to model the extent of damage and crater formation characteristics due to hypervelocity impacts on the rear wall of Aluminium multilayer shielding configuration. Close agreement was established between the numerical simulations and sourced experimental data, which show the effect of projectile density, impact velocity and spacing distance on the material degradation and debris plume.
AB - Numerical investigations into the complexities of hypervelocity impacts onto advanced aerospace structures provide an accurate description of the damage evolution and propagation through impacted structures. The accurate prediction of the dynamic behaviour and damage response upon hypervelocity impacts in microgravity enable an in-depth understanding of damage patterns in partially and fully damaged space structures. Numerical simulations using explicit finite elements codes were conducted to demonstrate the ability of Smoothed Particle Hydrodynamics to model the extent of damage and crater formation characteristics due to hypervelocity impacts on the rear wall of Aluminium multilayer shielding configuration. Close agreement was established between the numerical simulations and sourced experimental data, which show the effect of projectile density, impact velocity and spacing distance on the material degradation and debris plume.
UR - https://www.scopus.com/pages/publications/77953488962
M3 - Conference contribution
AN - SCOPUS:77953488962
SN - 9781615679089
T3 - 60th International Astronautical Congress 2009, IAC 2009
SP - 1925
EP - 1935
BT - 60th International Astronautical Congress 2009, IAC 2009
T2 - 60th International Astronautical Congress 2009, IAC 2009
Y2 - 12 October 2009 through 16 October 2009
ER -