Example 2: Lagrangian modeling for an impact problem 1 PREPARED BY NORI. NANAMI, TEXAS A & M UNIVERSITY EXAMPLE 2
2 PREPARED BY NORI. NANAMI, TEXAS A & M UNIVERSITY Direct impact problem A rigid body (5 kg) with 50 m/sec impacts on the aluminum plate. Aluminum plate Dimensions: 1m× 1m× 0.002m Material type: Linearly elastic behavior with isotropic hardening Element : Shell elements (S4R) Mesh size: 0.01m-0.05m Boundary condition: Four edges are fully constrained. Rigid body impactor Shape: cylinder with two hemispherical caps Dimensions: 0.32 in length × 0.16 m in a diameter Length/ diameter = 2 Initial bird mass: 5 kg Magnitude of initial velocity: VZ = -50 m/s Rigid elements (R3D4)
3 EXAMPLE 2 Target structure Model type: Shell model Shape: Square plate Dimensions: 1m× 1m PREPARED BY NORI. NANAMI, TEXAS A & M UNIVERSITY
4 EXAMPLE 2 PREPARED BY NORI. NANAMI, TEXAS A & M UNIVERSITY Reference geometry for an Impactor Model type: Discrete rigid model Shape: Cylinder with hemispherical cap and straight end Dimensions: 0.16 m in a diameter × 0.32 m in length
5 EXAMPLE 2 PREPARED BY NORI. NANAMI, TEXAS A & M UNIVERSITY
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7 PREPARED BY NORI. NANAMI, TEXAS A & M UNIVERSITY EXAMPLE 2 Coordinate (0,0,0) Coordinate (0.5, 0.5, 0.01)
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14 PREPARED BY NORI. NANAMI, TEXAS A & M UNIVERSITY EXAMPLE 2 Animation
15 PREPARED BY NORI. NANAMI, TEXAS A & M UNIVERSITY EXAMPLE 2 Target: 0 <X < 0.8 Animation
Lagrangian modeling is very traditional, available ABAQUS 6.12 documentation: Abaqus Analysis User's Manual “Rigid elements,” Section 30.3 ABAQUS 6.12 documentation: Abaqus Example Problems Manual “Rigid projectile impacting eroding plate,” Section PREPARED BY NORI. NANAMI, TEXAS A & M UNIVERSITY EXAMPLE 2