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Showing 1 to 1 of 1 for “"rocket combution chamber"”.

  1. Numerische Simulation des Wärmeübergangs in einer kryogenen Raketenbrennkammer

    … 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 turbulent effects were represented by the q-omega Low-Reynolds …

    aachen Repository record for Numerische Simulation des Wärmeübergangs in einer kryogenen Raketenbrennkammer (opens in a new tab)