Computational Study of the Kinetics of the Hydrogen-Oxygen Reaction Behind Steady State Shock Waves. Application to the Composition Limits and Transverse Stability of Gaseous Detonations

Computational Study of the Kinetics of the Hydrogen-Oxygen Reaction Behind Steady State Shock Waves. Application to the Composition Limits and Transverse Stability of Gaseous Detonations PDF Author: J. E. Dove
Publisher:
ISBN:
Category :
Languages : en
Pages : 12

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Book Description
The rate equations for the H2-O2 reaction have been integrated numerically under the conditions of steady flow in a Zeldovich-Doring-von Neumann detonation. A reaction scheme of 28 elementary reactions was used. The initial conditions covered the composition range from 16 to 92% H2 at pressures from 0.001 to 0.1 atm, 16 to 95 per cent at 1 atm, and 30 to 90 per cent at 10 atm. Comparison with the limited experimental data available shows that the computed induction times and reaction times are shorter than the experimental values. The reaction kinetic behavior of the H2-O2 system under conditions close to the isothermal branched-chain explosion limits is considered. The application to detonability limit calculations is discussed. (Author).

Computational Study of the Kinetics of the Hydrogen-Oxygen Reaction Behind Steady State Shock Waves. Application to the Composition Limits and Transverse Stability of Gaseous Detonations

Computational Study of the Kinetics of the Hydrogen-Oxygen Reaction Behind Steady State Shock Waves. Application to the Composition Limits and Transverse Stability of Gaseous Detonations PDF Author: J. E. Dove
Publisher:
ISBN:
Category :
Languages : en
Pages : 12

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Book Description
The rate equations for the H2-O2 reaction have been integrated numerically under the conditions of steady flow in a Zeldovich-Doring-von Neumann detonation. A reaction scheme of 28 elementary reactions was used. The initial conditions covered the composition range from 16 to 92% H2 at pressures from 0.001 to 0.1 atm, 16 to 95 per cent at 1 atm, and 30 to 90 per cent at 10 atm. Comparison with the limited experimental data available shows that the computed induction times and reaction times are shorter than the experimental values. The reaction kinetic behavior of the H2-O2 system under conditions close to the isothermal branched-chain explosion limits is considered. The application to detonability limit calculations is discussed. (Author).

Computational Study of Near-Limit Propagation of Detonation in Hydrogen-Air Mixtures

Computational Study of Near-Limit Propagation of Detonation in Hydrogen-Air Mixtures PDF Author: S. Yungster
Publisher:
ISBN:
Category :
Languages : en
Pages : 20

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Applied Mechanics Reviews

Applied Mechanics Reviews PDF Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 528

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History of Shock Waves, Explosions and Impact

History of Shock Waves, Explosions and Impact PDF Author: Peter O. K. Krehl
Publisher: Springer Science & Business Media
ISBN: 3540304215
Category : Science
Languages : en
Pages : 1298

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Book Description
This unique and encyclopedic reference work describes the evolution of the physics of modern shock wave and detonation from the earlier and classical percussion. The history of this complex process is first reviewed in a general survey. Subsequently, the subject is treated in more detail and the book is richly illustrated in the form of a picture gallery. This book is ideal for everyone professionally interested in shock wave phenomena.

Dynamics of Shock Waves, Explosions, and Detonations

Dynamics of Shock Waves, Explosions, and Detonations PDF Author: J. Raymond Bowen
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Category : Technology & Engineering
Languages : en
Pages : 632

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Proceedings

Proceedings PDF Author:
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Category : Engineering
Languages : en
Pages : 788

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Safety in Mines Abstracts

Safety in Mines Abstracts PDF Author:
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Category : Mine safety
Languages : en
Pages : 470

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International Aerospace Abstracts

International Aerospace Abstracts PDF Author:
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Category : Aeronautics
Languages : en
Pages : 898

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38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit: 02-3700 - 02-3749

38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit: 02-3700 - 02-3749 PDF Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 506

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Hydrogen Energy

Hydrogen Energy PDF Author:
Publisher:
ISBN:
Category : Hydrogen as fuel
Languages : en
Pages : 674

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