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Numerical Study on Unstable Combustion: Combustion Instability and Combustion Noise

Numerical Study on Unstable Combustion: Combustion Instability and Combustion Noise
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Mild Combustion

Progress in Energy and Combustion Science, 2004
The Mild Combustion is characterized by both an elevated temperature of reactants and low temperature increase in the combustion process. These features are the results of several technological demands coming from different application fields. This review paper aims to collect information which could be useful in understanding the fundamentals and ...
Cavaliere A, de Joannon M
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Combustion and CFD for Combustion

2010
The 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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Comparative combustion kinetics for in situ combustion process

Thermochimica Acta, 1999
Abstract 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 and Fuels

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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Combustion Processes in Mild Combustion

2005
Mild 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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Incomplete combustion - A possible cause of combustion instability

AIAA Journal, 1983
The 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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