An apparatus for improving heat transfer through a leading portion of an aircraft engine. The apparatus includes an annular channel that is defined by the leading portion. A source for gas that is fluidly connected to the channel and a narrow region that is defined within the annular channel.
Directed flow nozzle swirl enhancer
24.12.2019
Patent
Elektronische Ressource
Englisch
Kraftfahrwesen | 1981
|Evolution of swirl in two-dimensional-nozzle flow
AIAA | 1982
|