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An H.C.C.I. engine runs on a combustion process that researchers say holds the potential for significant gains in overall engine efficiency.
The thruster is based on a combustion chamber discharging a weight through an exhaust tube.
The results of material damping measurements performed on a beam specimen and on a combustion engine oil sump are presented.
A detailed kinetic model (303 species, 1922 reactions) based on a combustion model for light aromatic compounds has been extended to anisole.
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This method is based on the use of a combustion bomb calorimeter to determine the calorific values of the different samples studied.
At a motorbike high speed racing engine there is very important an output engine characteristics which depends significantly on a detonation combustion rate, atmospheric conditions and a combusted mixture composition.
Based on the measurement results, a combustion model for Estonian oil shale is proposed.
Since heat flux is a very important factor in designing cooling channels, the effects of recess length on heat flux in a combustion chamber must be carefully considered.
An experimental study has been carried out to study the effects of recess length in swirl coaxial injectors on heat transfer in a combustion chamber with cooling channels.
Similar behavior was reported by Colella, Majda, and Roytburd (SIAM J. Sci. Stat. Comput.7, 1059 (1986)) on a model combustion problem.
An optimal catalyst deposition technique was then developed for the preparation of premixed catalytic metal burners, which were tested on a pilot combustion chamber.
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