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Showing 1 to 1 of 1 for “"transport coefficients of mixtures"”.
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Numerische Simulation des Wärmeübergangs in einer kryogenen Raketenbrennkammer
The goal of this thesis is to determine the influence of different phenomena on the heat load of a hydrogen/oxygen rocket combustion chamber into the adjacent regenerative cooled wall. The heat transfer in turbulent flow is a result of turbulent vortices and the heat conductivity of the fluid. The …