Cost Comparison of Existing Coatings for a Hypervelocity Test Rail

Abstract

This study compared the relative costs, to the Department of Defense, of two different coatings used to protect a high speed test rail. Each coating was compared to the case of an uncoated rail with test conditions that caused catastrophic failure just after the test sled reached its maximum velocity. The total cost was finalized on a per test basis in order to sum cost of various expenditures that may only happen once every few tests. To compare the protective properties of each coating, various coated and uncoated samples were tested via a cylinder specimen Taylor Impact Test. Each coating's protective properties, or coating effectiveness, were found by its radial deformation change at the impacted end of each cylinder relative to the uncoated cylinder. This deformation change, relative to the uncoated cylinder's deformation, is the coating's effectiveness. Taylor Test results were then analyzed using the CTH hydrocode. CTH is able to model Taylor Impact Tests. CTH was used to understand the internal workings and results of the Taylor Tests in more depth. Verification between CTH and experimental Taylor Tests was done using final values for length, diameter and undeformed length of the cylinder.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 2005
Accession Number
ADA437725

Entities

People

  • Mark A. Blomer

Organizations

  • Air Force Institute of Technology

Tags

Communities of Interest

  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Boundary Layer
  • Computational Fluid Dynamics
  • Constitutive Equations
  • Department Of Defense
  • Diameters
  • Epoxy Coatings
  • Equations
  • Equations Of State
  • Fluid Dynamics
  • Hydrocodes
  • Impact Tests
  • Iron Oxides
  • Materials
  • Mechanics
  • Test Sets
  • Two Dimensional

Readers

  • Computational Fluid Dynamics (CFD)
  • Optical Fiber Sensing and Electromagnetic Propagation.
  • Structural Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow