Numerical Calculations of Hypervelocity Impact Crater Formation in Hard and Soft Aluminum Alloys,

Abstract

The wave propagation and crater growth characteristics in hypervelocity impact events on 1100-0 and 7075-T6 aluminum alloys are analyzed using a two-dimensional Eulerian numerical code called STEEP. The material model used in the calculations includes work hardening and thermal softening effects. Impacts of .635 cm aluminum spheres into semi-infinite targets at 7 km/sec and 4 km/sec are treated. Analytical predictions which can be compared directly with experimental results include crater growth characteristics and peak stress wave propagation and decay characteristics. Also included in the report are velocity field plots and principal stress field plots at selected times. The velocity magnitude, pressure, and normal stress are also plotted versus time at selected target locations. The numerical calculations show that material strength is important in determining the crater growth characteristics and final crater dimensions for the cases treated. (Author)

Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1971
Accession Number
AD0721468

Entities

People

  • M. Rosenblatt

Organizations

  • University of Dayton Research Institute

Tags

DTIC Thesaurus Topics

  • Alloys
  • Aluminum
  • Aluminum Alloys
  • Hardening
  • Hypervelocity Impact
  • Impact
  • Materials
  • Mechanical Properties
  • Softening
  • Stratified Fluids
  • Stress Waves
  • Stresses
  • Two Dimensional
  • Wave Propagation
  • Waves

Readers

  • Atmospheric Science / Meteorology, specifically Wind Wave Turbulence.
  • Computational Fluid Dynamics (CFD)
  • Explosive Engineering.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow