Time-dependent premixed deflagrations

Michael R. Booty

doi:10.2514/6.1996-910

Time-dependent premixed deflagrations

Michael R. Booty

Mathematical Sciences

Research output: Contribution to conference › Paper › peer-review

2 Scopus citations

Abstract

A reduced asymptotic model is formulated in the limit of small inverse nondimensional activation energy, ε — 0. to describe the time-dependent behavior of a class of premixed deflagrations. The model is similar to the reaction-sheet or flamelet models of combustion but the difference lies in the range of propagation Mach numbers considered, and here the initial Mach number A_io and ε satisfy the scaling relation M_i = O(ε). The reduced model requires numerical solution, and example results relevant to deflagration to detonation transition are presented for a configuration in which a deflagration in this class is situated between a driving piston and a preceding reactionless shock wave.

Original language	English (US)
DOIs	https://doi.org/10.2514/6.1996-910
State	Published - 1996
Event	34th Aerospace Sciences Meeting and Exhibit, 1996 - Reno, United States Duration: Jan 15 1996 → Jan 18 1996

Conference

Conference	34th Aerospace Sciences Meeting and Exhibit, 1996
Country/Territory	United States
City	Reno
Period	1/15/96 → 1/18/96

All Science Journal Classification (ASJC) codes

Space and Planetary Science
Aerospace Engineering

Access to Document

10.2514/6.1996-910

Cite this

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title = "Time-dependent premixed deflagrations",

abstract = "A reduced asymptotic model is formulated in the limit of small inverse nondimensional activation energy, ε — 0. to describe the time-dependent behavior of a class of premixed deflagrations. The model is similar to the reaction-sheet or flamelet models of combustion but the difference lies in the range of propagation Mach numbers considered, and here the initial Mach number Aio and ε satisfy the scaling relation Mi = O(ε). The reduced model requires numerical solution, and example results relevant to deflagration to detonation transition are presented for a configuration in which a deflagration in this class is situated between a driving piston and a preceding reactionless shock wave.",

author = "Booty, \{Michael R.\}",

note = "Publisher Copyright: {\textcopyright} 1996, by the American Institute of Aeronautics and Astronautics, Inc. All Rights Reserved.; 34th Aerospace Sciences Meeting and Exhibit, 1996 ; Conference date: 15-01-1996 Through 18-01-1996",

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AU - Booty, Michael R.

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N2 - A reduced asymptotic model is formulated in the limit of small inverse nondimensional activation energy, ε — 0. to describe the time-dependent behavior of a class of premixed deflagrations. The model is similar to the reaction-sheet or flamelet models of combustion but the difference lies in the range of propagation Mach numbers considered, and here the initial Mach number Aio and ε satisfy the scaling relation Mi = O(ε). The reduced model requires numerical solution, and example results relevant to deflagration to detonation transition are presented for a configuration in which a deflagration in this class is situated between a driving piston and a preceding reactionless shock wave.

AB - A reduced asymptotic model is formulated in the limit of small inverse nondimensional activation energy, ε — 0. to describe the time-dependent behavior of a class of premixed deflagrations. The model is similar to the reaction-sheet or flamelet models of combustion but the difference lies in the range of propagation Mach numbers considered, and here the initial Mach number Aio and ε satisfy the scaling relation Mi = O(ε). The reduced model requires numerical solution, and example results relevant to deflagration to detonation transition are presented for a configuration in which a deflagration in this class is situated between a driving piston and a preceding reactionless shock wave.

UR - https://www.scopus.com/pages/publications/85088769055

UR - https://www.scopus.com/pages/publications/85088769055#tab=citedBy

U2 - 10.2514/6.1996-910

DO - 10.2514/6.1996-910

M3 - Paper

AN - SCOPUS:85088769055

T2 - 34th Aerospace Sciences Meeting and Exhibit, 1996

Y2 - 15 January 1996 through 18 January 1996

ER -

Time-dependent premixed deflagrations

Abstract

Conference

All Science Journal Classification (ASJC) codes

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