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.
DIRECTIONAL FLOW NOZZLE SWIRL ENHANCER
DISPOSITF D'AMELIORATION DU TOURBILLON DE BUSE A FLUX DIRECTIONNEL
2017-11-02
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F28F Einzelheiten von Wärmetauschern oder Wärmeübertragungsvorrichtungen für allgemeine Verwendung , DETAILS OF HEAT-EXCHANGE OR HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION |
Automotive engineering | 1981
|Evolution of swirl in two-dimensional-nozzle flow
AIAA | 1982
|