Simulation of Impact Induced Detonation of AIM-120. A Novel Approach

Abstract

A high fidelity computational campaign was initiated to predict impact-induced detonation. The intent of this numerical simulation campaign is to capture dynamics and the intervening physical processes leading to detonation of AIM-12O Advanced Medium Range Air-to-Air Missile (AMRAAM) warhead (WDU-33/B) resulting from fragment impact. A new and innovative first principle calculational tool called "Smoothed Particle Hydrodynamics" (SPH) is used. SPH is an unstructured free Lagrangian hydrodynamic tool developed earlier to 2,3 for predicting consequences of high strain rate reaction processes where materials experience extreme density gradients and undergo large plastic deformation. Examples of such impulsive interactions can be found in penetration and fracture/fragmentation mechanics problems. Well-controlled field tests are conducted to verify the detonability of the AIM- 120 class missile warheads to high-speed fragment impacts. Detailed temporally and spatially varying fragment impact calculations are performed to illustrate the response of the AIM-120 to the kinetic energy of the impinging fragments. The correlation between calculational predictions and the field tests data are presented.

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1998
Accession Number
ADA379702

Entities

People

  • David F. Medina
  • Eric T. Olson
  • Firooz A. Allahdadi
  • Scott R. Jeffers

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Computational Fluid Dynamics
  • Computational Science
  • Continuum Mechanics
  • Detonations
  • Dynamics
  • Energetic Materials
  • Explosives
  • Failure Mode And Effect Analysis
  • Fluid Dynamics
  • Gruneisen Parameter
  • Hydrodynamics
  • Materials
  • Mechanics
  • Particles
  • Simulations
  • Three Dimensional
  • Two Dimensional

Readers

  • Computational Modeling and Simulation
  • Fluid Dynamics.
  • Rocket Propulsion.