Micro-explosive fragmentation of composite droplets: The effect of components of the aviation fuel; Chemical Engineering Science; Vol. 319

Dades bibliogràfiques
Parent link:Chemical Engineering Science.— .— Amsterdam: Elsevier Science Publishing Company Inc.
Vol. 319.— 2025.— Article number 122287, 17 p.
Altres autors: Antonov D. V. Dmitry Vladimirovich, Dolgikh V. V. Vladimir Viktorovich, Volokitin D. I. Dmitry Ivanovich, Vysokomornaya O. V. Olga Valeryevna
Sumari:Title screen
Experimental and theoretical research findings are reported on the characteristics of micro-explosive fragmentation of droplets containing water and aviation fuel components. Compositions with n-heptane, n-decane, n-dodecane and kerosene surrogate were used. Micro-explosive fragmentation delay times, duration and outcomes (secondary fragment sizes and increase in the evaporation surface area) of droplets were determined. These characteristics were compared with equivalent ones for raw and oxidized kerosene, rapeseed oil and diesel fuel. A verified mathematical model was used to predict the characteristics of micro-explosive fragmentation of fuel droplets containing up to 10 % water with initial sizes ranging from 10 µm to 1 mm and at a gas temperature between 500 K and 2000 K. Conditions were identified when it is appropriate to use model compositions based on components with dominant concentrations to predict the fragmentation characteristics of aviation fuels. It was also established when the precise composition of fuels should be taken into account
Текстовый файл
AM_Agreement
Idioma:anglès
Publicat: 2025
Matèries:
Accés en línia:https://doi.org/10.1016/j.ces.2025.122287
Format: MixedMaterials Electrònic Capítol de llibre
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=681746

MARC

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330 |a Experimental and theoretical research findings are reported on the characteristics of micro-explosive fragmentation of droplets containing water and aviation fuel components. Compositions with n-heptane, n-decane, n-dodecane and kerosene surrogate were used. Micro-explosive fragmentation delay times, duration and outcomes (secondary fragment sizes and increase in the evaporation surface area) of droplets were determined. These characteristics were compared with equivalent ones for raw and oxidized kerosene, rapeseed oil and diesel fuel. A verified mathematical model was used to predict the characteristics of micro-explosive fragmentation of fuel droplets containing up to 10 % water with initial sizes ranging from 10 µm to 1 mm and at a gas temperature between 500 K and 2000 K. Conditions were identified when it is appropriate to use model compositions based on components with dominant concentrations to predict the fragmentation characteristics of aviation fuels. It was also established when the precise composition of fuels should be taken into account 
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610 1 |a электронный ресурс 
610 1 |a труды учёных ТПУ 
610 1 |a Aviation fuel components 
610 1 |a Liquid fuels 
610 1 |a Alkanes 
610 1 |a Kerosene surrogate 
610 1 |a Micro-explosive fragmentation 
610 1 |a Secondary atomization of droplets 
701 1 |a Antonov  |b D. V.  |c specialist in the field of heat and power engineering  |c Associate Professor, Research Engineer at Tomsk Polytechnic University, Candidate of Physical and Mathematical Sciences  |f 1996-  |g Dmitry Vladimirovich  |9 22322 
701 1 |a Dolgikh  |b V. V.  |g Vladimir Viktorovich 
701 1 |a Volokitin  |b D. I.  |g Dmitry Ivanovich 
701 1 |a Vysokomornaya  |b O. V.  |c physicist  |c Associate Professor of Tomsk Polytechnic University, Candidate of Physical and Mathematical Sciences  |f 1984-  |g Olga Valeryevna  |9 17501 
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