A boundary layer control system includes a boundary layer separating portion that separates a boundary layer of an airflow at an underside of a body of a moving object from a main flow of the airflow, and an ejecting portion that ejects fluid in a state different from that of the boundary layer and the main flow, between the boundary layer and the main flow that have been separated by the boundary layer separating portion. This boundary layer control system is characterized in that boundary layer and the main flow are reliably separated by the fluid in a state different from that of the boundary layer and the main flow, so the percentage of the main flow that is slowed down (i.e., reduced in velocity) by the boundary layer is reduced.
BOUNDARY LAYER CONTROL SYSTEM
GRENZSCHICHTSTEUERSYSTEM
SYSTÈME DE COMMANDE DE COUCHE LIMITE
2017-02-15
Patent
Elektronische Ressource
Englisch
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