Zobrazeno 1 - 10
of 18
pro vyhledávání: '"B G Mingazov"'
Autor:
Yu. B. Aleksandrov, B. G. Mingazov
Publikováno v:
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 23, Iss 1, Pp 123-136 (2024)
A study of combustion characteristics in a swirling jet was carried out from the perspective of the theory of turbulent combustion. Particular attention is paid to the reverse-flow area formed from the vane swirler. Based on the known composition of
Externí odkaz:
https://doaj.org/article/02077106d08540fda5c128dae2485e9a
Publikováno v:
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 20, Iss 3, Pp 7-23 (2021)
The article proposes a method for designing combustion chambers for gas turbine engines based on a combination of the use of calculations in a one-dimensional and three-dimensional formulation of the problem. This technique allows you to quickly desi
Externí odkaz:
https://doaj.org/article/6fdfb0b56b0a45c5af4d23af4b91625f
Autor:
T. D. Nguyen, B. G. Mingazov
Publikováno v:
Russian Aeronautics. 64:736-741
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::79982d2ecfedf6b93bc6edf683b4c072
https://doi.org/10.3103/s106879982104019x
https://doi.org/10.3103/s106879982104019x
Publikováno v:
Russian Aeronautics. 64:268-276
The paper presents the method of studying the fuel combustion and typical characteristics of biogas combustion process obtained in experiments. The main factors influencing the flame stability and the laminar combustion velocity in the biogas flow ar
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::11e91304fb28c0a869f9348224e76e11
https://doi.org/10.3103/s1068799821020148
https://doi.org/10.3103/s1068799821020148
Publikováno v:
Russian Aeronautics. 63:669-676
The paper investigates the swirling flow behind the GTE combustion chamber swirler with blades installed under different angles. The mixing ratio in the flow is experimentally analyzed and compared with the estimated values obtained by a numerical ap
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9c13197cdc61f5da81aace46707c55d5
https://doi.org/10.3103/s1068799820040145
https://doi.org/10.3103/s1068799820040145
Autor:
B. G. Mingazov, A. V. Baklanov
Publikováno v:
Russian Aeronautics. 63:469-475
The results are presented of the experimental and computational studies of the flame stabilization behind a swirler in an open flow and in a model compartment of the combustion chamber. Using the thermal theory, the calculation model of the flame sta
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::45556cc74bc3c661f598a25b81613bac
https://doi.org/10.3103/s1068799820030137
https://doi.org/10.3103/s1068799820030137
Autor:
B. G. Mingazov, T. Kh. Mukhametgaliev
Publikováno v:
Russian Aeronautics. 63:101-104
The mechanism of flame stabilization in phase-inhomogeneous air—fuel mixtures is considered. A method is proposed for refining the thermal theory of flame stabilization by taking into account the heat consumed for heating and evaporation liquid fue
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ad0dfc4aa69616b413a443cc2170d222
https://doi.org/10.3103/s1068799820010146
https://doi.org/10.3103/s1068799820010146
Publikováno v:
Russian Aeronautics. 62:281-286
A mixing process is simulated and a calculation technique for determining the mixing ratio is created based on experimental studies. Influence of some factors on this ratio is determined in the recirculation mixing zone in the swirling flow behind th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2f8e5af2c6081b71cade4800eea8ba82
https://doi.org/10.3103/s1068799819020156
https://doi.org/10.3103/s1068799819020156
Publikováno v:
AIP Conference Proceedings.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c00f95a64c1392960682b783d5966979
https://doi.org/10.1063/5.0003049
https://doi.org/10.1063/5.0003049
Publikováno v:
Russian Aeronautics. 60:406-411
As a result of the experimental-theoretical study of the loop (countercurrent) combustion chamber of the gas turbine engine, the data and theoretical dependences are obtained on the change in the combustion completeness and combustion temperature in
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e84eb2c143bd73a14415caaadbe42b13
https://doi.org/10.3103/s1068799817030126
https://doi.org/10.3103/s1068799817030126