Modeling a High Speed Pin-on-Disc Experiment by Comparison of Numerical Solutions to a Moving Boundary Nonlinear Heat Equation

Abstract

The purpose of this work is to analyze the heat transfer characteristics of VascomaxC300 during high-speed sliding. This work extends previous research that is intended to help predict the wear-rate of connecting shoes for a hypersonic rail system at Holloman Air Force Base. Solutions were generated using finite element analysis, finite difference methods, and spectral methods. The frictional heat generated by the pin-on-disc is assumed to flow uniformly and normal to the face of the pin and the pin is assumed to be a perfect cylinder resulting in two-dimensional heat flow. Displacement data obtained from the experiment is used to define the moving boundary. The distribution of temperature resulting from transient finite element analysis is used to justify a one-dimensional model. The one dimensional heat equation is solved with variable parameters using a variable-step, variable-order, implicit finite-difference method. Spectral methods are then employed to calculate the spatial derivatives improving the approximation of the function which represents the data. It is concluded that a one-dimensional approach with constant heat transfer parameters sufficiently models the high-speed pin-on-disc experiment.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 2021
Accession Number
AD1132635

Entities

People

  • Aron R Wing

Organizations

  • Air Force Institute of Technology

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Air Force Research Laboratories
  • Applied Mathematics
  • Computational Science
  • Difference Equations
  • Differential Equations
  • Energy
  • Energy Transfer
  • Engineering
  • Equations
  • Finite Element Analysis
  • Heat Energy
  • Heat Transfer
  • Heat Transmission
  • Materials
  • Partial Differential Equations
  • Standards
  • Thermal Conductivity
  • Thermal Diffusivity
  • Two Dimensional
  • United States Government

Readers

  • Finite Element Method (FEM) for solving Partial Differential Equations (PDEs)
  • Fluid Dynamics.
  • ballistics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow