Affiliation:
1. Scientific and Educational Centre of Fluid Dynamics Research, Samara National Research University, Samara, Russia
Abstract
The purpose of this paper is to conduct experimental research of hazardous substance emissions at the simulated combustion chamber output. The experiment was carried in a simulated combustion chamber. The combustion chamber included a burner device; a liquid fuel feed system; and a flame tube with two rows of mixing holes and one row of cooling holes. The combustion chamber operation mode was φ = 0.435, Tpreheat = 423 K, and the atmospheric pressure. The liquid fuel burn rate was 0.77 g/s. The pressure ratio in the combustion chamber remained constant at ΔP = 3%. Two types of fuel were used: aviation kerosene of Russia’s TS-1 brand and the fuel surrogate was n-decane mixture (C10H22) with benzene additions (C6H6). The benzene additions were 5% through 30% (n-decane/benzene: 95/5, 90/10, 85/15, 80/20, 75/25, and 70/30).
Funder
Ministry of Education and Science of the Russian Federation
Subject
Energy Engineering and Power Technology,Condensed Matter Physics,Fuel Technology,General Chemical Engineering
Cited by
4 articles.
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1. Modelling of multi-component kerosene and surrogate fuel droplet heating and evaporation characteristics: A comparative analysis;Fuel;2020-06
2. Study of the formation of polycyclic aromatic hydrocarbons in the combustion chambers of aircraft engines;INTERNATIONAL CONFERENCE ON PHYSICS AND CHEMISTRY OF COMBUSTION AND PROCESSES IN EXTREME ENVIRONMENTS (COMPHYSCHEM’20-21) and VI INTERNATIONAL SUMMER SCHOOL “MODERN QUANTUM CHEMISTRY METHODS IN APPLICATIONS”;2020
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4. Simulation of CO and CO2 emissions in model combustion chamber based on the combination LES and Reactor Network model;E3S Web of Conferences;2019