Active flow separation control using synthetic jet actuators /

The use of synthetic jet actuators for controlling the boundary layer flow and flow separation over a wing is investigated. A theory for the optimum design of actuators using motors is developed. A motor driven synthetic jet actuator is built and validated for separation control in the water tunnel....

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Bibliographic Details

Main Author:	Rao, Preetham P.
Format:	Thesis eBook
Language:	English
Published:	[Place of publication not identified] : [publisher not identified] ; 2000.
Subjects:	Major aerospace engineering.
Online Access:	Link to OAKTrust copy