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Accurate measurement data for film cooling with gaseous hydrogen are presented and discussed which were obtained with a novel rectangular, experimental combustion chamber. Furthermore, a new correlation for the prediction of film cooling efficiency is introduced showing good agreement with experimental data.
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This page is a summary of: Heat Transport Processes of Gaseous Film Cooling in Rocket Combustion Chambers, Journal of Thermophysics and Heat Transfer, October 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.t7095.
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