Synopsis of a Theory for Shock Impedance Effects in a Rough-Walled Tunnel

Abstract

The paper postulates five related impedance mechanisms that control the propagation of blast wave through a rough-walled tunnel: entry diffraction, build-up, turbulent choke, wall roughness, and feedback. These combined impedance mechanisms from rough walls rapidly reduce tunnel overpressures down to structurally manageable levels (approx. = 1 bar) within the first few dozen lengths L/D, almost independently of surface pressure near the entry. A relatively slow decrease in tunnel pressures occurs beyond L/D = 50 or at low pressures (< 1 bar). Excellent correlation--within 20 percent--is found with measurements made in rough-walled shock tubes. A program in simple BASIC machine language (suitable for time-sharing teletype) summarizes the calculations, permits the user to input any surface pressure and wall roughness desired, and prints an annotated tabular history of shock pressure down the tunnel. Classic idealizations, such as one-dimensional analyses, or experiments close to the entrance of a smooth-walled tunnel are not considered usually relevant to these phenomena.

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1967
Accession Number
AD0653860

Entities

People

  • Francis B. Porzel

Organizations

  • Institute for Defense Analyses

Tags

Communities of Interest

  • Advanced Electronics
  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Absorption Coefficients
  • Angle Of Incidence
  • Blast
  • Blast Waves
  • Boundary Layer
  • Engineering
  • Flow
  • High Pressure
  • Kinetic Energy
  • Layers
  • Materials
  • Measurement
  • Shock Tubes
  • Surface Burst
  • Surface Roughness
  • Turbulent Flow
  • Waves

Fields of Study

  • Physics

Readers

  • Combustion Dynamics and Shock Wave Physics.
  • Fluid Dynamics.