Steady State Stress in a Coated Infinite Half-Space Subjected to a Moving Load

Abstract

This research investigates the use of coatings to mitigate the stress distribution into an infinite half-space. High energy impact phenomenon at velocities exceeding the speed of sound is an important area of interest to the Air Force Research Laboratory. Holloman Air Force Base's High Speed Test Track sustains significant damage due to this phenomenon. In this thesis, the track system and coating are modeled analytically with equations of motion in terms of linear displacements. Coating thickness and material properties of epoxy or polymer laminates are investigated to understand their affect of stress distribution in the rail. An analytic solution is used to verify a finite difference method. It is found that due to limitations in coating thickness of the track system, this property has no significant affect on the stress distribution. However, the shear modulus of the material is found to have a significant affect representing the possible onset of material failure through the consideration of the combined stress field at the coating-rail interface.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 2005
Accession Number
ADA434400

Entities

People

  • Jason M. Cruthirds

Organizations

  • Air Force Institute of Technology

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Coordinate Systems
  • Difference Equations
  • Differential Equations
  • Displacement
  • Equations
  • Equations Of Motion
  • Geometry
  • High Energy
  • Materials
  • Mechanics
  • Modulus Of Elasticity
  • Shear Modulus
  • Shear Stresses
  • Steady State
  • Stress Waves
  • Thickness

Readers

  • Calculus or Mathematical Analysis
  • Reinforced Composite Materials

Technology Areas

  • Space