Сибирский федеральный университет

Тип публикации: доклад, тезисы доклада, статья из сборника материалов конференций

Конференция: Siberian Thermophysical Seminar (STS); Russian Acad Sci, SB, Kutateladze Inst Thermophys, Novosibirsk, RUSSIA; Russian Acad Sci, SB, Kutateladze Inst Thermophys, Novosibirsk, RUSSIA

Год издания: 2019

Идентификатор DOI: 10.1088/1742-6596/1382/1/012059

Аннотация: This paper reports on the investigation of combustion features of synthesis gas/air and methane/air flames in a model gas turbine combustor with swirling flow via numerical simulation. This combustor developed for experimental investigation of flow, heat transfer and combustion. For synthesis gas combustion ratio of hydrogen and carbon monoxide was 1:1. The equivalence ratio Φ in both cases was 1.5. The combustor contains systems for water- and air-cooling that provides reasonable temperature value of combustor walls in operating mode. The methane/air flame has the lifted V-shape and synthesis gas/air flame has the columnar tubular flame. In practical, the V-shape flames are more often used. To provide more practical combustion regimes for synthesis gas/air mixture it is necessary to increase the fuel-oxidant mixing efficiency in the premixer of the combustor. © 2019 Published under licence by IOP Publishing Ltd.

Журнал: Journal of Physics: Conference Series

Выпуск журнала: Vol. 1382, Is. 1

Номера страниц: 12059

ISSN журнала: 17426588

Издатель: Institute of Physics Publishing

• Lobasov A.S. (RAS, Siberian Branch, Kutateladze Inst Thermophys, 1 Lavrentyev Ave, Novosibirsk 630090, Russia; Novosibirsk State Univ, 2 Pirogova St, Novosibirsk 630090, Russia)
• Dekterev Ar A. (RAS, Siberian Branch, Kutateladze Inst Thermophys, 1 Lavrentyev Ave, Novosibirsk 630090, Russia)
• Minakov A.V (RAS, Siberian Branch, Kutateladze Inst Thermophys, 1 Lavrentyev Ave, Novosibirsk 630090, Russia; Siberian Fed Univ, 79 Svobodny Pr, Krasnoyarsk 660041, Russia)

• Scopus
• Web of Science Core Collection
• Ядро РИНЦ (eLIBRARY.RU)