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Algorithms for Reaction Mechanism Reduction and Numerical Simulation of Detonations Initiated by Projectiles

Hung, Patrick (2003) Algorithms for Reaction Mechanism Reduction and Numerical Simulation of Detonations Initiated by Projectiles. PhD thesis, California Institute of Technology. https://resolver.caltech.edu/CaltechCACR:2003.208

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Abstract

The evolution of a homogeneous, chemically reactive system with ns species forms a dy-namical system in chemical state-space. Under suitable constraints, unique and stable equi-librium exists and can be interpreted as zeroth-dimensional (point like) attractors in this ns-dimensional space. At these equilibrium compositions, the rates of all reversible reac-tions vanish and can, in fact, be determined from thermodynamics independent of chemical kinetics. Generalizing this concept, an m-dimensional Intrinsic Low Dimensional Manifold (ILDM) represents an m-dimensional subspace in chemical state-space where all but the m-slowest aggregate reactions are in equilibrium, and these aggregate reactions are determined by eigenvalue considerations of the chemical kinetics. In this context, a certain composition is said to be m-dimensional if it is on an m-, but not an (m – 1)-, dimensional ILDM. Two new algorithms are proposed that allow the dimensionality of chemical composi-tions be determined simply. The first method is based on recasting the Maas and Pope algorithm. The second, and more efficient, method is inspired by the mathematical struc-ture of the Maas and Pope algorithm and makes use of the technique known as arc-length reparameterization. In addition, a new algorithm for the construction of ILDM, and the application of these ideas to detonation simulations, is discussed. In the second part of the thesis, numerical simulations of detonation waves initiated by hypervelocity projectiles are presented. Using detailed kinetics, only the shock-induced com-bustion regime is realized as simulating the conditions required for a stabilized detonation is beyond the reach of our current computational resources. Resorting to a one-step irre-versible reaction model, the transition from shock-induced combustion to stabilized oblique detonation is observed, and an analysis of this transition based on the critical decay-rate model of Kaneshige (1999) is presented.


Item Type:Thesis (PhD)
Related URLs:
URLURL TypeDescription
https://resolver.caltech.edu/CaltechETD:etd-05302003-142744Related ItemPhD Dissertation
https://resolver.caltech.edu/CaltechAUTHORS:20230209-225908701Related ItemASCI Technical Report
Additional Information:Also available in the Caltech Center for Simulation of Dynamic Response in Materials publication series, cit-asci-tr190, at http://csdrm.caltech.edu/publications/index.html
Group:Center for Advanced Computing Research
Record Number:CaltechCACR:2003.208
Persistent URL:https://resolver.caltech.edu/CaltechCACR:2003.208
Usage Policy:You are granted permission for individual, educational, research and non-commercial reproduction, distribution, display and performance of this work in any format.
ID Code:28205
Collection:CaltechCACR
Deposited By: Imported from CaltechCACR
Deposited On:18 Jan 2005
Last Modified:09 Feb 2023 23:04

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