THE MECHANISM OF THE TRANSITION FROM DEFLAGRATION TO DETONATION IN HIGH EXPLOSIVES

Abstract

Experimental results of the study of spontaneous transition from deflagration to detonation indicate that the approach to the problem can be in two stages; the first is the formation of a shock from pressure waves engendered by a confined deflagration, and the second the shock-initiation of detonation. A program for the analytical treatment of the first stage was written for the IBM 704. Two numerical codes have been tested, one based on the so-called q- method and one which avoids amplitude fluctuations inherent in the q-method and thus gives a more realistic representation of a shock wave. Representations of spontaneous shock formation obtained by the two numerical codes and by the analytical treatment are discussed and compared. The numerical methods yield the temperature as a function of time and location during growth of the shock and thus allow a study of simple chemical kinetic models. Introduction of chemical kinetics into the program gives a basis for elucidation of the second stage of the transition problem, namely shock-initiation of detonation.

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Document Details

Document Type
Technical Report
Publication Date
Apr 14, 1961
Accession Number
AD0256593

Entities

People

  • Carl T. Zovko

Organizations

  • Naval Ordnance Laboratory

Tags

Communities of Interest

  • Air Platforms
  • Counter IED
  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aeronautical Engineering
  • Aircrafts
  • Chemical Kinetics
  • Chemical Reactions
  • Differential Equations
  • Equations
  • Equations Of Motion
  • Explosions
  • Explosives
  • Fluid Dynamics
  • High Explosives
  • Materials Laboratories
  • Mechanics
  • Munitions
  • Ordnance Laboratories
  • Physics
  • Physics Laboratories

Fields of Study

  • Physics

Readers

  • Finite Element Method (FEM) for solving Partial Differential Equations (PDEs)
  • Rocket Propulsion.
  • Underwater engineering and Marine Technology.