Various Finite Difference Schemes for Transient Three Dimensional Heat Conduction,

Abstract

The motivation for this task comes from the needs of future hypervelocity projectile surrounded by asymmetric flow due to angle of attack and/or fins in case of kinetic energy projectile. In either case, unsteady and three-dimensional effects, large and nonuniform heat fluxes, tedious and repetitive number crunching capabilities of supercomputers dictate optimum numerical techniques and predictive critical time steps for successful and practical solutions. Finite element modeling is ideal whenever there is geometrical complexity, coatings, composite and multi materials. However, classical finite element technique yields a particular equation. There may be some finite difference schemes superior to classical finite element technique. Therefore, various finite difference schemes are derived and their characteristics are discussed applicable to transient three dimensional heat conduction problems.

Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1992
Accession Number
ADP006610

Entities

People

  • Rao Yalamanchili
  • Surya R. Yalamanchili

Organizations

  • United States Army Armament Research, Development and Engineering Center

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Applied Mathematics
  • Composite Materials
  • Equations
  • Heat Flux
  • Hypervelocity Projectiles
  • Kinetic Energy
  • Kinetic Energy Projectiles
  • Materials
  • Mathematics
  • Projectiles
  • Three Dimensional

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Structural Dynamics.
  • Systems Analysis and Design

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight