Published December 1999 | Version public
Journal Article

The chemical-gas dynamic mechanisms of pulsating detonation wave instability

  • 1. ROR icon University of Illinois Urbana-Champaign
  • 2. ROR icon Rensselaer Polytechnic Institute
  • 3. ROR icon California Institute of Technology

Abstract

The chemical–gas dynamic mechanisms behind the instability and failure of a one–dimensional pulsating detonation wave driven by a three–step chain–branching reaction are revealed by direct numerical simulation. Two types of pulsating instability observed experimentally are explained. The first involves regular oscillations of the detonation front, where the instability is driven by low–frequency finite–amplitude compression and expansion waves in the chain–branching induction zone between the main reaction layer and the detonation shock. For irregular oscillations of the front, the instability mechanism first involves a decoupling between the shock and main reaction layer. Subsequently, the main reaction layer accelerates, drives a compression wave ahead of it, and undergoes a transition to detonation. This internal detonation wave overtakes the lead detonation shock, generating a new high–pressure detonation, which rapidly decays. A smaller–amplitude pressure oscillation occurs during the decay with a mechanism reminiscent of that observed for the previous regular oscillation, before the detonation and main reaction layer once again decouple and the instability cycle is repeated. For failure scenarios, the shock temperature is observed to drop to the cross–over temperature for the chain–branching reaction, causing the main reaction layer to decouple and retreat indefinitely from the detonation shock.

Additional Information

© 1999 The Royal Society. Published online: 01/12/1999; published in print: 01/12/1999. M.S. was supported by the US Air Force Office of Scientific Research, Mathematics (F49620-96-1-0260). A.K.K. was supported by the Los Alamos National Laboratory and by the National Science Foundation.

Additional details

Identifiers

Eprint ID
107109
Resolver ID
CaltechAUTHORS:20201215-163507736

Funding

Air Force Office of Scientific Research (AFOSR)
F49620-96-1-0260
Los Alamos National Laboratory
NSF

Dates

Created
2020-12-16
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Updated
2021-11-16
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