PENETRATION OF STRUCTURES BY HYPERVELOCITY PROJECTILES,

Abstract

During the early stages after impact by a hypervelocity projectile, the cratering process in the target is very nearly governed by the hydrodynamic model except near the edge of the forming cavity. A mathematical model, supported in detail by numerical solutions of the defining partial differential equations, is valid at all axial positions of the peak pressure pulse beyond that point where this pulse is first attenuated by edge rarefaction fronts proceeding from the projectile periphery from the moment of impact. This point occurs a fraction of a microsecond after impact. A detailed study of various impacting metals is made and the theory presented here shows that in the hypervelocity regime a thick target sees no essential difference between geometrically similar projectiles of like material impacting at a given kinetic energy. (Author)

Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1964
Accession Number
AD0431199

Entities

People

  • J. F. Heyda
  • T. D. Riney

Organizations

  • General Electric

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundaries
  • Cratering
  • Differential Equations
  • Energy
  • Equations
  • Hypervelocity Projectiles
  • Kinetic Energy
  • Materials
  • Mathematical Models
  • Mathematics
  • Microsecond Time
  • Models
  • Partial Differential Equations
  • Projectiles
  • Rarefaction

Fields of Study

  • Physics

Readers

  • Combustion Dynamics and Shock Wave Physics.
  • Explosive Engineering.
  • Finite Element Method (FEM) for solving Partial Differential Equations (PDEs)

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight