Effect of lid height and blowing ratio on film cooling effectiveness of a novel lidded hole configuration
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DOI: 10.1177/09544089221095665
Abstract: Film cooling is one of the promising technologies used for protecting rocket nozzles and turbine blades from combustion chamber hot gases. This paper proposes a novel shape of film cooling injection hole, called lidded hole,… read more here.
Keywords: lidded hole; cooling effectiveness; hole configuration; film cooling ... See more keywords