Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Yu. G. Kutsenko"'
Autor:
V. G. Avgustinovich, Yu. G. Kutsenko
Publikováno v:
Russian Aeronautics (Iz VUZ). 54:170-178
A two-front model of turbulent combustion is presented, which makes it possible to describe the processes taking place in diffusive and homogeneous flame fronts, as well as to take into account the influence of various factors that cause flame front
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9dec03b5998d5e3a0cddc36504d30f22
https://doi.org/10.3103/s1068799811020103
https://doi.org/10.3103/s1068799811020103
Autor:
Yu. G. Kutsenko
Publikováno v:
Russian Aeronautics (Iz VUZ). 52:208-213
A modification of the Zimont turbulent combustion model is presented; the modification makes it possible to describe processes in diffusion and homogeneous flame fronts as well as to take into account the influence of different factors that cause fla
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2a578759091b8dc9831811f6ebadeba9
https://doi.org/10.3103/s1068799809020123
https://doi.org/10.3103/s1068799809020123
Publikováno v:
Volume 2: Combustion, Fuels and Emissions.
Most of the modern combustor’s designs use staged concepts for reducing thermal NO emissions. Usually, a combustion process takes place inside the main zone, which uses very lean premixed fuel/air mixtures. A diffusion pilot zone supports combustio
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::def2f94ad8fcbfc872c06c4a2d80e55c
https://doi.org/10.1115/gt2009-60131
https://doi.org/10.1115/gt2009-60131
Publikováno v:
Volume 3: Combustion, Fuels and Emissions, Parts A and B.
Most of the modern combustor’s designs use staged concepts for reducing thermal NO emissions. Usually, a combustion process takes place inside the main zone, which uses very lean premixed fuel/air mixtures. A diffusion pilot zone supports combustio
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::026a7a69e844b29dab534704cac36626
https://doi.org/10.1115/gt2008-50289
https://doi.org/10.1115/gt2008-50289
Publikováno v:
Volume 2: Turbo Expo 2007.
Modern concepts for reducing thermal NO emissions require the use of very lean fuel/air mixtures. Therefore a problem of lean quench should be solved during design process of gas turbine combustor and it’s operational development. Since maintenance
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c17338a6beec225ea1ba6f09afd1bc60
https://doi.org/10.1115/gt2007-27699
https://doi.org/10.1115/gt2007-27699
Autor:
Yu. G. Kutsenko, S. F. Onegin
Publikováno v:
Volume 1: Combustion and Fuels, Education.
A combustor is a crucial unit of gas turbine engine because it should work reliably at high temperatures; provide a suitable temperature distribution at entry to the turbine and supply a low emission level of harmful substances. An operational develo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e4457dd177c1414eee1981f7b8f38104
https://doi.org/10.1115/gt2006-90530
https://doi.org/10.1115/gt2006-90530