Three-Dimensional Oblique Shock Diffraction Over a Rectangular Parallelepiped: Computational/Experimental Comparison

Abstract

Three-dimensional, unsteady finite-difference calculations with the HULL hydrocode are used to describe the shock diffraction process resulting from a shock wave striking the front of a scaled model of an S-280 Electrical Equipment shelter at oblique incidence. The 52.5 degree obliquity of the incident 34.5 kPa (5 psi) overpressure shock on the front face produces a peak reflected overpressure that is approximately 50 percent larger than that for normal reflection. The numerical calculations are discussed and evaluated by comparison with experimental pressure measurements taken in shock tube tests on a scale-model shelter. Difficulties are experienced in both the 3-D calculations and the experiment in resolving the peak reflected overpressure on the front face. Except for some disagreement in the values for peak overpressure on the shelter front and windward side faces, the comparisons between computed and experimentally measured pressure for all faces show good agreement. Three- dimensional and two-dimensional cell-size convergence studies are discussed which quantify the influence of cell size on the numerical results.

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1982
Accession Number
ADA122254

Entities

People

  • Brian P. Bertrand
  • Clarence W. Kitchens Jr.
  • John D. Wortman
  • Richard E. Lottero

Organizations

  • Ballistic Research Laboratory

Tags

Communities of Interest

  • Counter WMD
  • Energy and Power Technologies
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Angle Of Incidence
  • Cell Size
  • Engineering
  • Experimental Data
  • Flow Fields
  • Fluid Dynamics
  • Frequency
  • Frequency Response
  • Leading Edges
  • Military Research
  • National Security
  • Plastic Explosives
  • Pressure Gages
  • Pressure Measurement
  • Three Dimensional
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Combustion Dynamics and Shock Wave Physics.
  • Computational Fluid Dynamics (CFD)
  • Explosive Engineering.