{"title":"The thermodynamics of C-J deflagration","authors":"Yunfeng Liu","doi":"10.1016/j.csite.2024.105574","DOIUrl":null,"url":null,"abstract":"The mechanisms of detonation instability, detonation quenching, deflagration-to-detonation transition, and thermodynamics of C-J deflagration are fundamental issues of combustion theory. In this paper, these mechanisms are discussed by analyzing the convective flux and heat release flux of one-dimensional numerical simulation. The governing equations are Euler equation with overall one-step chemical reaction kinetics. The mixture is stochiometric H<ce:inf loc=\"post\">2</ce:inf>-air mixture at 1atm and 300K.The activation energy is increased to trigger the instability of C-J detonation. The numerical results show that the detonation instability is induced by the von Neumann spike. The von Neumann spike produces unsteady rarefaction wave, which is determined by the slope of von Neumann spike. The detonation is extinguished to a C-J deflagration abruptly under critical activation energy at one-time step because the strength of rarefaction wave is stronger than heat release under this critical condition. The C-J deflagration propagates with a relative constant velocity about half of C-J detonation velocity. The gas temperature and pressure behind the leading shock wave of C-J deflagration is too low to ignite the mixture. The Taylor wave from the end-wall ceases the mixture behind the leading shock, increases its temperature and decreases its pressure. As a result, combustion takes place at the contact surface with almost constant pressure. Therefore, the C-J deflagration is of constant-pressure combustion and this mechanism makes it propagate downstream with a relatively constant velocity for a long distance.","PeriodicalId":9658,"journal":{"name":"Case Studies in Thermal Engineering","volume":"13 1","pages":""},"PeriodicalIF":6.4000,"publicationDate":"2024-11-26","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Case Studies in Thermal Engineering","FirstCategoryId":"5","ListUrlMain":"https://doi.org/10.1016/j.csite.2024.105574","RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"THERMODYNAMICS","Score":null,"Total":0}
引用次数: 0
Abstract
The mechanisms of detonation instability, detonation quenching, deflagration-to-detonation transition, and thermodynamics of C-J deflagration are fundamental issues of combustion theory. In this paper, these mechanisms are discussed by analyzing the convective flux and heat release flux of one-dimensional numerical simulation. The governing equations are Euler equation with overall one-step chemical reaction kinetics. The mixture is stochiometric H2-air mixture at 1atm and 300K.The activation energy is increased to trigger the instability of C-J detonation. The numerical results show that the detonation instability is induced by the von Neumann spike. The von Neumann spike produces unsteady rarefaction wave, which is determined by the slope of von Neumann spike. The detonation is extinguished to a C-J deflagration abruptly under critical activation energy at one-time step because the strength of rarefaction wave is stronger than heat release under this critical condition. The C-J deflagration propagates with a relative constant velocity about half of C-J detonation velocity. The gas temperature and pressure behind the leading shock wave of C-J deflagration is too low to ignite the mixture. The Taylor wave from the end-wall ceases the mixture behind the leading shock, increases its temperature and decreases its pressure. As a result, combustion takes place at the contact surface with almost constant pressure. Therefore, the C-J deflagration is of constant-pressure combustion and this mechanism makes it propagate downstream with a relatively constant velocity for a long distance.
期刊介绍:
Case Studies in Thermal Engineering provides a forum for the rapid publication of short, structured Case Studies in Thermal Engineering and related Short Communications. It provides an essential compendium of case studies for researchers and practitioners in the field of thermal engineering and others who are interested in aspects of thermal engineering cases that could affect other engineering processes. The journal not only publishes new and novel case studies, but also provides a forum for the publication of high quality descriptions of classic thermal engineering problems. The scope of the journal includes case studies of thermal engineering problems in components, devices and systems using existing experimental and numerical techniques in the areas of mechanical, aerospace, chemical, medical, thermal management for electronics, heat exchangers, regeneration, solar thermal energy, thermal storage, building energy conservation, and power generation. Case studies of thermal problems in other areas will also be considered.