Lumbar load attenuation for rotorcraft occupants using a design methodology for the seat impact energy-absorbing system

Articles in the same Issue

1. Forward to special issue on blast and impact of engineering structures
2. Shape optimization of high-speed penetrators: a review
3. High velocity impact on composite link of aircraft wing flap mechanism
4. On pulse pressure loading of plates with holes
5. Dynamic response of sandwich shells to underwater blasts
6. Impact damage assessment by using peridynamic theory
7. Modelling and simulation of explosions in soil interacting with deformable structures
8. Damage progression from impact in layered glass modeled with peridynamics
9. Lumbar load attenuation for rotorcraft occupants using a design methodology for the seat impact energy-absorbing system
10. Experimental and numerical analysis of stress wave propagation in polymers and the role of interfaces in armour systems
11. Modelling and analysis of vehicle crash system integrated with different VDCS under high speed impacts
12. Damage evolution in GLARE fibre-metal laminate under repeated low-velocity impact tests
13. Delamination of impacted composite structures by cohesive zone interface elements and tiebreak contact
14. An investigation on low-velocity impact response of elastomeric & crushable foams
15. Experimental and analytical study of high velocity impact on Kevlar/Epoxy composite plates
16. Ultrasonic detection of spall damage induced by low-velocity repeated impact
17. Experimental analysis and simulation of effective factors on explosive forming of spherical vessel using prefabricated four cones vessel structures