Zobrazeno 1 - 5
of 5
pro vyhledávání: '"V. A. Sychenkov"'
Publikováno v:
Russian Aeronautics. 64:277-282
A technique is presented for calculating the main parameters along the flame tube length in the combustor with combustion of premixed air–fuel mixtures. The calculation in the combustion zone is carried out by numerical solution of the system of eq
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2db445c0e58faa539ff9066c4a0e5500
https://doi.org/10.3103/s106879982102015x
https://doi.org/10.3103/s106879982102015x
Publikováno v:
Russian Aeronautics. 61:64-70
This paper presents the results of an investigation of ejectors with the low entrainment ratio. A technique for calculating the ejectors with a curvilinear axis has been developed. Comparative studies of the performance characteristics of ejectors wi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::561b437e2620dc7a0d267065d5e68829
https://doi.org/10.3103/s1068799818010105
https://doi.org/10.3103/s1068799818010105
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
Publikováno v:
Russian Aeronautics (Iz VUZ). 57:141-147
In this paper, the results of investigating a coaxial gas ejector without increase of passive flow pressure are presented. A technique for calculation of coaxial ejectors has been developed. This investigation has resulted in the optimal structure of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::daacad3e448093e000458e2785e428aa
https://doi.org/10.3103/s1068799814020056
https://doi.org/10.3103/s1068799814020056
Publikováno v:
Russian Aeronautics (Iz VUZ). 51:90-93
A scheme of the nozzle blade arrangement in the two-stage GTE turbine is described taking into account peripheral periodic inhomogeneity of the temperature field.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f7f9d0aa8e3e9d7c9c2e0b60995ad520
https://doi.org/10.3103/s1068799808010157
https://doi.org/10.3103/s1068799808010157