Wave Motion in Low-Pressure-Ratio Rectangular and Pyramidal Shock Tubes,

Abstract

Closed-form solutions based on acoustic theory have recently been obtained to describe the wave motion in both low-pressure-ratio rectangular (constant area) and pyramidal shock tubes which utilize different driver and channel gases. These new solutions are in excellent agreement with experimental data. This work should be of interest to researchers who are using shock tubes or similar devices to produce impulse noise, in particular the similated sonic boom, in order to facilitate studies of the effects of impulse sound on humans, animals and structures. Furthermore, this work is relevant to the understanding of the wave motion produced by weak planar and spherical explosions of finite size. (Author)

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1975
Accession Number
ADA040148

Entities

People

  • James Joseph Gottlieb

Organizations

  • University of Toronto

Tags

Communities of Interest

  • Advanced Electronics

DTIC Thesaurus Topics

  • Acoustic Waves
  • Agreements
  • Air Force
  • Barometric Pressure
  • Carbon Dioxide
  • Dielectric Gases
  • Differential Equations
  • Digital Computers
  • Experimental Data
  • Far Field
  • Noise
  • Shock Tubes
  • Shock Waves
  • Simulators
  • Sonic Boom
  • Three Dimensional
  • Tubes

Readers

  • Electromagnetic Wave Scattering and Antenna Radiation Engineering
  • Fluid Dynamics.
  • Theoretical Analysis.