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reactive material; shaped charge jet; trans-scale discretization; formation; unsaturated clay; moisture content; Hugoniot parameters; high-pressure EOS; multi-diameter tungsten fiber-reinforced Zr-based bulk metallic glasses matrix composite; tungsten fiber; penetration failure mode; bend space; ultimate bending diameter; explosively formed projectile; tungsten heavy alloy; liner material; dynamic response; fracture mechanics; Johnson–Kendall–Robert model; polyurethane setae array; surface energy; modeling; simulation; reactive materials; impact-induced deflagration; ignition behavior; reaction ratio; temperature distribution; dynamic modeling; impact; kinetic projectile; honeycomb; multi-layer plates; dynamic model; weaved composite material; unmanned aerial vehicle; parachute recovery; deployment phase; parameter analysis; fine-grained D6A steel; fine grain strengthening; strain rate sensitivity; Johnson–Cook constitutive model; finite element simulation; ceramic composite armor; 12.7 mm API projectile; ballistic performance; deflection and yaw; NM500/Q345 clad plate; austenitization; microstructure; properties; movement; inclusions; cold hearth; flow field; PTFE/Al; Johnson-Cook constitutive model; reactive shaped charge jet; numerical simulation; near-α titanium alloy; dynamic deformation; deformation twin; Johnson–Cook equation; reactive materials projectile; multi-layer aluminum target; damage evolutionary behavior; deflagration reaction; n/a