Numerical simulation of secondary combustion of hydrogen injected from preburner into supersonic airflow

AIAA Journal ◽  
1997 ◽  
Vol 35 ◽  
pp. 1441-1447
Author(s):  
Sadegh Tabejamaat ◽  
Yiguang Ju ◽  
Takashi Niioka
Keyword(s):  
Numerical Simulation ◽  
Secondary Combustion ◽  
Supersonic Airflow ◽  
Combustion Of Hydrogen

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 Supersonic Airflow with Transverse Hydrogen Injection

2001 ◽  
Vol 17 (6) ◽  
pp. 1319-1326 ◽  
Author(s):  
E. von Lavante ◽  
D. Zeitz ◽  
M. Kallenberg
Keyword(s):  
Numerical Simulation ◽  
Supersonic Airflow
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