Theoretical Studies of Detonation Waves

Abstract

Theoretical studies of reactive shock waves were performed to obtain a fundamental understanding of the initiation and propagation of detonation in condensed explosives. The differential equation governing a shock discontinuity was used to determine different conditions associated with a single shock trajectory for build-up to detonation. One of these conditions was used to construct the type of flow observed in PBX 9404 during the early stages of initiation produced by a flying plate. Various aspects of initiation induced by a constant velocity piston were considered. Equations relating the initial flow to the initial energy release rate were derived. Conditions were also determined for the shock to accelerate with either a positive or a negative pressure gradient. These conditions demonstrate how the mechanism of initiation depends on the energy release rate, the sound speed, and on the relationship between these quantities. A critical energy was defined for waves that build up to detonation with a positive particle velocity gradient. Work on the reactive shock problem was continued and integral relationships for unsteady flow were derived as generalized Rankine-Hugoniot equations without making approximations.

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1978
Accession Number
ADA060614

Entities

People

  • Clarence M. Ablow
  • Craig M. Tarver
  • Michael Cowperthwaite

Organizations

  • SRI International

Tags

Communities of Interest

  • Counter IED
  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Acoustic Propagation
  • Chemical Reactions
  • Detonation Waves
  • Detonations
  • Differential Equations
  • Equations
  • Equations Of State
  • Exothermic Reactions
  • Explosions
  • Explosives
  • Military Research
  • Plastic Bonded Explosives
  • Pressure Gradients
  • Steady State
  • Stratified Fluids
  • Thermodynamics
  • Unsteady Flow

Readers

  • Calculus or Mathematical Analysis
  • Combustion Dynamics and Shock Wave Physics.