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Combustion and CFD for Combustion
2010The following chapters present an overview of combustion and of CFD (Computational Fluid Dynamics) for combustion. The objective is not to repeat classical textbooks on these topics [379; 306; 288; 334; 340] but to focus on the place of instabilities in reacting flows and in CFD for reacting flows.
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Application of the first combustion model to spray combustion
Applied Thermal Engineering, 2004Liquid fuel is of interest to apply to gas turbines. The large advantage is that liquids are easily storable as compared to gaseous fuels. Disadvantage is that liquid fuel has to be sprayed, vaporized and mixed with air. Combustion occurs at some stage of mixing and ignition.
de Jager, B., Kok, J.B.W.
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Comparative combustion kinetics for in situ combustion process
Thermochimica Acta, 1999Abstract In this research, thermal characteristics and combustion kinetics of three crude oils (13–27°API) were investigated using DuPont 9900 thermal analysis system (TG/DTG). A sample size of 10 mg, heating rate of 10°C min −1 were used in the temperature range of 20–700°C under air atmosphere.
M. V. Kök, C. Ö. Keskin
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Combustion Processes in Mild Combustion
2005Mild Combustion is a process completely different both from deflagration, detonation, explosion in a classic form, and also from the processes that generate diffusion flames. Therefore it deserves to be analyzed separately from these processes and quoted with a specific name.
A Cavaliere, M de Joannon
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1985
The fundamental difference between spark ignition (SI) and compression ignition (CI) engines lies in the type of combustion that occurs, and not in whether the process is idealised as an Otto cycle or a Diesel cycle. The combustion process occurs at neither constant volume (Otto cycle), nor constant pressure (Diesel cycle).
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The fundamental difference between spark ignition (SI) and compression ignition (CI) engines lies in the type of combustion that occurs, and not in whether the process is idealised as an Otto cycle or a Diesel cycle. The combustion process occurs at neither constant volume (Otto cycle), nor constant pressure (Diesel cycle).
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Incomplete combustion - A possible cause of combustion instability
AIAA Journal, 1983The performance of and the combustion in solid-propellant rocket motors may be affected by characteristic length \((L^*)\). For small characteristic lengths, the chamber pressure and characteristic velocity may be lower than in similar motors with larger \(L^*\). Oscillatory combustion may take place if the \(L^*\) is small enough. In the past, \(L^*\)
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The combustion process and combustion analysis
2021Anthony J. Martyr, David R. Rogers
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2010
Mild Combustion processes evolve in a temperature and concentration range outside the limit of interest of standard combustion processes, with the aim of lowering the maximum temperature of the whole process below the value at which massive pollutants formation occurs.
Mariarosaria de Joannon +2 more
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Mild Combustion processes evolve in a temperature and concentration range outside the limit of interest of standard combustion processes, with the aim of lowering the maximum temperature of the whole process below the value at which massive pollutants formation occurs.
Mariarosaria de Joannon +2 more
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2003
The book can be downloaded from www.combustion.tue.nl/course/lecturenotes ...
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The book can be downloaded from www.combustion.tue.nl/course/lecturenotes ...
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