What is it about?
The structure of rocket engines has to withstand massive heat loads. This is not possible without the application of cooling techniques. One possible way of protecting the structure is the use of film cooling. We investigated this technique experimentally under almost realistic rocket-engine-like conditions.
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This page is a summary of: Experimental Investigations of Film Cooling in a Conical Nozzle Under Rocket-Engine-Like Flow Conditions, AIAA Journal, March 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j057486.
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