THEORY OF HIGH SPEED IMPACT

Abstract

Results of hypervelocity impact tests were gathered and the composite data are presented. The extrapolated results to higher velocities differ with the theoretical prediction from the perfect fluid model. A visco-plastic model for hypervelocity impact is formulated. This is accomplished by introducing a viscosity factor mu sub o and a yield stress tau sub a into the perfect fluid equations. The equations governing the visco-plastic model are studied. Certain dimensionless parameters are found which determine the relative importance of the inertial, viscous and plastic effects during the various stages of the hypervelocity cratering process. To exhibit quantitatively the importance of including the viscous and plastic effects, a one-dimensional impact model was studied. The values of mu sub o and tau sub a are varied since definitive data are available for neither parameter in the hypervelocity range. Two distinct finite difference schemes were developed for performing the required calculations. The results are related to the qualitative model of crater formations that evolved from experimental studies in which the actual cratering process was monitored. The viscous and strength effects strongly affect the cavitation process which is the essential mechanism of crater formation.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1962
Accession Number
AD0274048

Entities

People

  • T. D. Riney

Organizations

  • General Electric

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Accuracy
  • Air Force
  • Aluminum Alloys
  • Axisymmetric Flow
  • Difference Equations
  • Differential Equations
  • Experimental Data
  • Hydrodynamics
  • Mechanics
  • Modulus Of Elasticity
  • New York
  • Numerical Analysis
  • Partial Differential Equations
  • Shear Stresses
  • Space Systems
  • Spacecraft
  • Two Dimensional

Readers

  • Combustion Dynamics and Shock Wave Physics.
  • Computational Modeling and Simulation
  • Explosive Engineering.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight
  • Hypersonics - Hypersonic Flow