Explicit dynamic formulation to demonstrate compliance against quasi-static aircraft seat certification loads (CS25.561) - Part II: Influence of body blocks

Keyphrases

• Kinematics 100%
• Explicit Dynamic Method 100%
• Aircraft Seat 100%
• Automobile Seat 100%
• Quasi-static 100%
• Body Block 100%
• Seat Certification 100%
• Dynamic Integration 50%
• Quasi-static Response 50%
• Explicit Code 50%
• Nonlinear Problems 50%
• Certification Requirements 50%
• Numerical Results 50%
• Quality Check 50%
• Integration Scheme 50%
• Quasi-static Solution 50%
• Element Distortion 50%
• Solution Accuracy 50%
• All Elements 50%
• Aerospace 50%
• Slippery Liquid-Infused Porous Surfaces (SLIPS) 50%
• Convergence Issues 50%
• LS-DYNA3D 50%
• Nonlinear Quasi-static Analysis 50%
• Explicit Finite Element Analysis 50%
• Procedural 50%
• Error Checking 50%
• Explicit Integration Scheme 50%
• Verification Framework 50%
• Courant-Friedrichs-Lewy Condition 50%
• Load Case 50%
• Computer-aided Engineering 50%
• Large Deformation 50%
• Computation Time 50%
• Loading Effect 50%
• Loading Mechanism 50%
• Implicit Solver 50%
• Time Scaling 50%
• Mass Scaling 50%
• Explicit Dynamics 50%
• Highly Nonlinear 50%
• Modeling Approach 50%

Engineering

• Aircraft Seats 100%
• Automotives 100%
• Demonstrate Compliance 100%
• Computer Aided Engineering 50%
• Element Distortion 50%
• Mass Damping 50%
• Nonlinear Problem 50%
• Converged Solution 50%
• Large Deformation 50%
• Computational Time 50%
• Belts 50%
• Finite Element Analysis 50%
• Implicit Solver 50%
• Static Response 50%
• Mass Block 50%
• Computer Aided Design 50%
• Energy Engineering 50%
• Load Case 50%
• Review Paper 50%
• Static Solution 50%
• Static Analysis 50%