Isothermal modeling of swirling flow aerodynamic structure in a two-stage burner
The work motivation is determined by the extensive use of interacting swirling flows in counter vortex quenchers and vortex combustion chambers. To optimize the design of such devices, it is necessary to understand the structure of the flow and the mechanisms of interaction of co
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Format: | Article |
Language: | Russian |
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Tomsk Polytechnic University
2017-08-01
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Series: | Известия Томского политехнического университета: Инжиниринг георесурсов |
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Online Access: | http://izvestiya-tpu.ru/archive/article/view/1899 |
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author | Sergey Ivanovich Shtork Roman Ravilevich Yusupov Sergey Vladimirovich Alekseenko |
author_facet | Sergey Ivanovich Shtork Roman Ravilevich Yusupov Sergey Vladimirovich Alekseenko |
author_sort | Sergey Ivanovich Shtork |
collection | DOAJ |
description | The work motivation is determined by the extensive use of interacting swirling flows in counter vortex quenchers and vortex combustion chambers. To optimize the design of such devices, it is necessary to understand the structure of the flow and the mechanisms of interaction of co |
first_indexed | 2024-03-13T07:37:31Z |
format | Article |
id | doaj.art-434c47935d9742c2b542e82356560718 |
institution | Directory Open Access Journal |
issn | 2500-1019 2413-1830 |
language | Russian |
last_indexed | 2024-03-13T07:37:31Z |
publishDate | 2017-08-01 |
publisher | Tomsk Polytechnic University |
record_format | Article |
series | Известия Томского политехнического университета: Инжиниринг георесурсов |
spelling | doaj.art-434c47935d9742c2b542e823565607182023-06-03T21:12:24ZrusTomsk Polytechnic UniversityИзвестия Томского политехнического университета: Инжиниринг георесурсов2500-10192413-18302017-08-013287Isothermal modeling of swirling flow aerodynamic structure in a two-stage burnerSergey Ivanovich ShtorkRoman Ravilevich YusupovSergey Vladimirovich AlekseenkoThe work motivation is determined by the extensive use of interacting swirling flows in counter vortex quenchers and vortex combustion chambers. To optimize the design of such devices, it is necessary to understand the structure of the flow and the mechanisms of interaction of cohttp://izvestiya-tpu.ru/archive/article/view/1899vortex burnerscoaxial swirling flowshigh-speed visualizationlaser-Doppler anemometerprecessing vortex core |
spellingShingle | Sergey Ivanovich Shtork Roman Ravilevich Yusupov Sergey Vladimirovich Alekseenko Isothermal modeling of swirling flow aerodynamic structure in a two-stage burner Известия Томского политехнического университета: Инжиниринг георесурсов vortex burners coaxial swirling flows high-speed visualization laser-Doppler anemometer precessing vortex core |
title | Isothermal modeling of swirling flow aerodynamic structure in a two-stage burner |
title_full | Isothermal modeling of swirling flow aerodynamic structure in a two-stage burner |
title_fullStr | Isothermal modeling of swirling flow aerodynamic structure in a two-stage burner |
title_full_unstemmed | Isothermal modeling of swirling flow aerodynamic structure in a two-stage burner |
title_short | Isothermal modeling of swirling flow aerodynamic structure in a two-stage burner |
title_sort | isothermal modeling of swirling flow aerodynamic structure in a two stage burner |
topic | vortex burners coaxial swirling flows high-speed visualization laser-Doppler anemometer precessing vortex core |
url | http://izvestiya-tpu.ru/archive/article/view/1899 |
work_keys_str_mv | AT sergeyivanovichshtork isothermalmodelingofswirlingflowaerodynamicstructureinatwostageburner AT romanravilevichyusupov isothermalmodelingofswirlingflowaerodynamicstructureinatwostageburner AT sergeyvladimirovichalekseenko isothermalmodelingofswirlingflowaerodynamicstructureinatwostageburner |