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5 - Droplets and Particles: Evaporation in High-Temperature Flow and Combustion in Boundary Layers

from Part II - Mathematical Modeling of Selected Typical Modes of Combustion

Published online by Cambridge University Press:  16 August 2019

V. I. Naoumov ,
V. G. Krioukov ,
A. L. Abdullin  and
A. V. Demin
V. I. Naoumov
Affiliation:
Central Connecticut State University
V. G. Krioukov
Affiliation:
Kazan National Research Technical University, Russian Federation
A. L. Abdullin
Affiliation:
The Academy of Science of the Republic of Tatarstan, Russian Federation
A. V. Demin
Affiliation:
Kazan State Power Engineering University, Russian Federation
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Summary

Evaporation and combustion of dispersed propellants in a high-temperature reacting flow are typical for the most diverse propulsion and power generation systems such as internal combustion engines (ICE), combustors of air breathing engines (ABE), combustion chambers of liquid-propellant rocket engines (LPRE), liquid gas generators (LGG), and steam-gas generators (SGG), combustion chambers of furnaces, etc. Liquid-propellant atomization, spray formation, and droplet evaporation processes are seen to bear strong influence on the efficiency of the combustion process and, hence, the operating and ecological parameters of these combustion systems.

Type
Chapter
Information
Chemical Kinetics in Combustion and Reactive Flows
Modeling Tools and Applications
 , pp. 228 - 261
Publisher: Cambridge University Press
Print publication year: 2019

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