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
Keyword(s):  
Numerical Simulation ◽  
Fuel Injection ◽  
Hydrocarbon Fuel ◽  
Gaseous Hydrocarbon ◽  
Hypersonic Inlet

Effects of supercritical environment on hydrocarbon-fuel injection

2017 ◽  
Vol 26 (2) ◽  
pp. 183-191 ◽  
Author(s):  
Bongchul Shin ◽  
Dohun Kim ◽  
Min Son ◽  
Jaye Koo
Keyword(s):  
Fuel Injection ◽  
Hydrocarbon Fuel

SPECTRAL DIAGNOSTICS OF THE HYDROCARBON FUEL COMBUSTION PROCESS

2021 ◽  
pp. 12-17
Author(s):  
M. A. Vaganov
Keyword(s):  
Combustion Process ◽  
Hydrocarbon Fuel ◽  
Combustion Products ◽  
Combustible Mixture ◽  
Fuel Combustion ◽  
Propane Combustion ◽  
Gaseous Hydrocarbon ◽  
Spectral Bands ◽  
Air Supply ◽  
Spectral Diagnostics

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.

Numerical Simulation on Hypersonic Combustion of Hydrogen-Fueled Scramjet Combustor with Parallel Strut Fuel Injection at a Flight Mach Number of 7

2015 ◽  
Vol 766-767 ◽  
pp. 1044-1049
Keyword(s):  
Numerical Simulation ◽  
Mach Number ◽  
Numerical Investigation ◽  
Fuel Injection ◽  
International Space ◽  
Scramjet Combustor ◽  
Combustion Of Hydrogen

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

Numerical simulation of hypersonic inlet flows

1998 ◽  
Author(s):  
J. van Keuk ◽  
J. Ballmann ◽  
A. Schneider ◽  
W. Koschel
Keyword(s):  
Numerical Simulation ◽  
Hypersonic Inlet

Real gas effects on the numerical simulation of a hypersonic inlet

1986 ◽  
Vol 2 (4) ◽  
pp. 381-382 ◽  
Author(s):  
Wing-Fai Ng ◽  
Thomas J. Benson ◽  
William G. Kunik
Keyword(s):  
Numerical Simulation ◽  
Real Gas ◽  
Hypersonic Inlet ◽  
Real Gas Effects

Numerical simulation of hypersonic inlet flows with equilibrium or finite rate chemistry

1988 ◽  
Author(s):  
SHENG-TAO YU ◽  
KWANG-CHUNG HSIEH ◽  
JIAN-SHUN SHUEN ◽  
BONNIEJ. MCBRIDE
Keyword(s):  
Numerical Simulation ◽  
Finite Rate ◽  
Hypersonic Inlet
Sign in / Sign up

Export Citation Format

Share Document