Tables and Graphs of the Theoretical Peak Pressures, Energies, and Positive Impulses of Blast Waves in Air

Abstract

A theory of the propagation of shock waves from explosive sources was presented in OSRD Report No. 4814. In that report, a pair of ordinary differential equations for peak pressure and shock-wave energy as functions of the distance from the source were formulated from the equations of hydrodynamics by imposing a similarity restraint on the shape of the energy-time curve of the shock wave. Two-parameter families of peak pressure-distance, shock-wave energy-distance, and positive impulse-distance curves are obtained by the solution of these propagation equations. The parameters are conveniently chosen as the initial values of the pressure and shock-wave energy. In the present report, tables and graphs of the two-parameter families of curves for blast waves from explosive sources in air are presented. A method is outlined for the determination of the parameters from experimental values of the peak pressure and positive impulse over a limited range of distances from the source. Estimates of the properties of the blast wave produced by TNT are obtained in this manner, and tentative peak pressure-distance and impulse-distance curves for all distances from the charge are constructed.

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1945
Accession Number
ADB807901

Entities

People

  • John G. Kirkwood
  • S. R. Brinkley Jr.

Organizations

  • Cornell University

Tags

Communities of Interest

  • Counter IED
  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Abstracts
  • Afterburning
  • Blast
  • Blast Waves
  • Differential Equations
  • Energy
  • Equations
  • Explosions
  • Explosive Charges
  • Explosives
  • Land Mines
  • Measurement
  • Munitions
  • National Security
  • Scientific Research
  • Shock Waves
  • Wave Power

Fields of Study

  • Physics

Readers

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