Numerical Simulation of Gaseous Hydrocarbon Fuel Injection in a Hypersonic Inlet

2010 ◽  
Vol 26 (5) ◽  
pp. 1114-1124 ◽  
Author(s):  
Yen-W. Wang ◽  
Jean P. Sislian
2017 ◽  
Vol 26 (2) ◽  
pp. 183-191 ◽  
Author(s):  
Bongchul Shin ◽  
Dohun Kim ◽  
Min Son ◽  
Jaye Koo

2021 ◽  
pp. 12-17
Author(s):  
M. A. Vaganov

It is proposed to use the methods of applied optical spectroscopy to solve the problem of control and diagnostics of gaseous hydrocarbon fuel combustion in this work. The results of an experimental study of spectroscopic informative parameters characterizing the propane combustion process are presented for three modes: combustion of pure propane without air supply, stoichiometric combustion and combustion with a change in the amount of supplied air relative to stoichiometric combustion. As a result of the experiment, it was found that the most intense bands in the emission spectrum of the flame arising from the combustion of propane correspond to the spectral bands of radicals of combustion products: OH, CH, and C2. While the intensities of various systems of bands in the flame spectrum depend significantly on the composition of the combustible mixture.


2015 ◽  
Vol 766-767 ◽  
pp. 1044-1049

Removed due to plagiarism. The original was published as: Numerical Investigation of Inlet-Combustor Interactions for a Scramjet Hydrogen-Fueled Engine at a Flight Mach number of 8. Authors: Edder Rabadan and Bernhard Weigand 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, Tours, France, 2012. Paper ID AIAA-2012-5926, DOI: 10.2514/6.2012-5926


1998 ◽  
Author(s):  
J. van Keuk ◽  
J. Ballmann ◽  
A. Schneider ◽  
W. Koschel

1986 ◽  
Vol 2 (4) ◽  
pp. 381-382 ◽  
Author(s):  
Wing-Fai Ng ◽  
Thomas J. Benson ◽  
William G. Kunik

1988 ◽  
Author(s):  
SHENG-TAO YU ◽  
KWANG-CHUNG HSIEH ◽  
JIAN-SHUN SHUEN ◽  
BONNIEJ. MCBRIDE

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