In this paper, analytical modeling and numerical simulation of sandwich panel behavior with metal foam
core under low impact impact are presented and how the formation and development of impact defects in
impact loading conditions in three samples with different face sizes Taken, checked. Multi-layer sandwich
panels are made of epoxy carbon and the core is also made of metal foam. Analytical modeling of low speed
shock load on sandwich panels, using mass model and two-degree free spring, has been used to calculate
the contact force. The spring stiffness of the contact site, and the bending and shear spring stiffness of the
sandwich panel are calculated, the values of which change over time. To solve the equations of motion, the
exact solution method has been used and the radius of the affected area is calculated using energy
equations. In the next section, simulation of low speed impact on sandwich panels with metal foam core is
done in three samples of different sizes in Abacus software, so that we see how to create and develop defects
in sandwich panels. In the next section, we have examined the results and compared the numerical solution
and analytical simulation, which confirms the process of research and this has been proven to be important.