Numerical Simulation of Supersonic Nonpremixed Turbulent Combustion in a Scramjet Combustor Model

2010 ◽  
Vol 26 (4) ◽  
pp. 858-868 ◽  
Author(s):  
Arnaud Mura ◽  
Jean-Francois Izard
Keyword(s):  
Numerical Simulation ◽  
Turbulent Combustion ◽  
Scramjet Combustor

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 model scramjet combustor flowfield

2007 ◽  
Vol 36 (5) ◽  
pp. 295-302
Author(s):  
Yuan-Guang Wang ◽  
Xu Xu ◽  
Guo-Biao Cai
Keyword(s):  
Numerical Simulation ◽  
Scramjet Combustor

Theoretical Investigation and Numerical Simulation of Turbulent Combustion in an Industrial Combustor With Combustion Gases Recirculation

2004 ◽  
Author(s):  
Kunpeng Zhang ◽  
Fei Xue ◽  
Weiming Pan
Keyword(s):  
Numerical Simulation ◽  
Physical Model ◽  
Active Control ◽  
Theoretical Investigation ◽  
Turbulent Combustion ◽  
Thermodynamic Investigation ◽  
Combustion Gases ◽  
Calculation Results ◽  
Ejector System

Thermodynamic investigation was conducted to study the role of ejector system in a CGR (Combustion Gases Recirculation) combustor. Physical model was established to evaluate the intensity of CGR and the confirmed relationship between CGR and gas ejection was found. In order to validate the theory analyses, an industry combustor with CGR was modeled. The calculation results accord with the theory analyses. All the results implied that Active Control Combustion (ACC) might be implemented with control of gas ejection.

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