scholarly journals Cooling Performance Analysis of Regeneratively Cooled Combustion Chamber

2004 ◽  
Vol 32 (4) ◽  
pp. 67-72
Keyword(s):  
Performance Analysis ◽  
Combustion Chamber ◽  
Cooling Performance

Cooling Performance Analysis of Heat Sink

2011 ◽  
Vol 1 (9) ◽  
pp. 65-67
Author(s):  
Pritesh S Patel ◽  
◽  
Prof. Dattatraya G Subhedar ◽  
Prof. Kamlesh V Chauhan
Keyword(s):  
Performance Analysis ◽  
Heat Sink ◽  
Cooling Performance

1225 Modeling for Cooling Performance Analysis of Active Magnetic Refrigerator

2010 ◽  
Vol 2010.85 (0) ◽  
pp. _12-25_
Author(s):  
Yu MIYAOKA ◽  
Tsuyoshi KAWANAMI ◽  
Shigeki HIRANO ◽  
Shigeki HIRASAWA ◽  
Elyas Fauzi Bin Salleh Fauzi
Keyword(s):  
Performance Analysis ◽  
Cooling Performance ◽  
Magnetic Refrigerator

scholarly journals Performance analysis of turbofan engine with additional combustion chamber fueled by alternative fuel

2019 ◽  
Vol 179 (4) ◽  
pp. 249-253
Author(s):  
Natalia MARSZAŁEK
Keyword(s):  
Performance Analysis ◽  
Combustion Chamber ◽  
Alternative Fuels ◽  
Engine Performance ◽  
Alternative Fuel ◽  
Positive Influence ◽  
Aviation Fuel ◽  
Turbofan Engine ◽  
Low Pressure Turbine ◽  
Liquid Methane

Presented paper is focused on the performance analysis of turbofan engine with additional combustion chamber fueled by alternative fuel. Additional combustion chamber was situated between high pressure turbine and low pressure turbine. Such configuration is also know under the name inter turbine burner (ITB). As an alternative fuels burn in additional combustion chamber were selected cryogenics fuels: liquid hydrogen and liquid methane. The main combustion chamber was supplied by conventional aviation fuel - kerosene. Thermodynamic model of turbofan engine with ITB was implemented in MATLAB environment. The problem of modeling an additional combustion chamber was presented.Analysis was carried out for take-off conditions. Obtained results indicate that implementation of ITB exert a positive influence on engine performance result in thrust increase.

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