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Applied Mathematics and Mechanics in Aerospace Industry Read chapter Read first chapter

2021 | OriginalPaper | Chapter

8. Some Aspects on Pulsating Detonation Wave Numerical Simulation Using Detailed Chemical Kinetics Mechanism

Author : Alexander I. Lopato

Published in: Applied Mathematics and Computational Mechanics for Smart Applications

Publisher: Springer Singapore

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Abstract

The chapter is dedicated to the numerical study of pulsating gaseous detonation wave propagation. The mathematical model is based on the Euler equations written for the multicomponent gas and supplemented by the detailed chemical reactions model to describe the combustion of the hydrogen–air mixture. The Petersen and Hanson kinetics is applied as the detailed chemical model. The numerical algorithm is based on the finite volume approach, essentially non-oscillatory scheme, AUSM numerical flux and the Runge–Kutta method. The numerical investigation of pulsating detonation wave propagation with direct detonation initiation near the closed end of the channel is carried out. The peculiarities of high-frequency and high-amplitude pulsations modes are discussed.

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previous chapter Numerical Simulation of Generation, Distribution, and Impact of a High-Specific Energy Plasma Bunch on a Barrier
next chapter A Godunov-Type Method for a Multi-temperature Plasma with Strong Shock Waves and a General Equation of State
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Metadata
Title
Some Aspects on Pulsating Detonation Wave Numerical Simulation Using Detailed Chemical Kinetics Mechanism
Author
Alexander I. Lopato
Copyright Year
2021
Publisher
Springer Singapore
Book
Applied Mathematics and Computational Mechanics for Smart Applications

Print ISBN: 978-981-334-825-7

Electronic ISBN: 978-981-334-826-4

Copyright Year: 2021

DOI
https://doi.org/10.1007/978-981-33-4826-4_8

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