Mathematical modeling and experimental investigations of oxygen-methane fuel combustion at coaxial-jet supply into the combustion chamber of liquid-propellant rocket engine |
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Authors: | V R Rubinskii S P Khrisanfov V Yu Klimov A V Kretinin |
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Institution: | 1.OAO KB Khimavtomatiki,Voronezh,Russia;2.Voronezh State Technical University,Voronezh,Russia |
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Abstract: | The numerical results are presented for the case of coaxial-jet supply at the different ratio of mass component velocities
at the combustion chamber inlet with the constant and variable relationship of oxygen-methane components. The experimental
investigations of coaxial-jet mixing elements as part of the model setup chamber operating on corrosive producer gas and gaseous
methane were carried out. A qualitative pattern of the $
\overline {\rho u}
$
\overline {\rho u}
parameter influence on the chamber economic feasibility was obtained: as $
\overline {\rho u}
$
\overline {\rho u}
decreases, the combustion efficiency coefficient grows. |
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Keywords: | |
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