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dc.creatorOryu, Hiroshi
dc.date.accessioned2012-06-07T23:00:42Z
dc.date.available2012-06-07T23:00:42Z
dc.date.created2000
dc.date.issued2000
dc.identifier.urihttps://hdl.handle.net/1969.1/ETD-TAMU-2000-THESIS-O79
dc.descriptionDue to the character of the original source materials and the nature of batch digitization, quality control issues may be present in this document. Please report any quality issues you encounter to digital@library.tamu.edu, referencing the URI of the item.en
dc.descriptionIncludes bibliographical references (leaves 48-50).en
dc.descriptionIssued also on microfiche from Lange Micrographics.en
dc.description.abstractA feasibility study of utilizing synthetic jet actuators as a mean to mitigate disturbances that can cause instability and turbulent flow is described. Prediction of flow transition via linear stability theory was performed by solving the Orr-Sommerfeld equation. The development of a sensor-actuator control system unit using synthetic jet actuators for flow transition control was studied. The implementation of the disturbance generator using a DC motor for the generation of a desired frequency of the disturbance was conducted. The target frequency and the corresponding free stream speed were chosen according to the linear stability theory. The implementation of the open-loop actuator controller was studied. Test operations of tracking the reference signal were examined. The study of the open-loop sensor-actuator controller including a hot film sensor was conducted.en
dc.format.mediumelectronicen
dc.format.mimetypeapplication/pdf
dc.language.isoen_US
dc.publisherTexas A&M University
dc.rightsThis thesis was part of a retrospective digitization project authorized by the Texas A&M University Libraries in 2008. Copyright remains vested with the author(s). It is the user's responsibility to secure permission from the copyright holder(s) for re-use of the work beyond the provision of Fair Use.en
dc.subjectaerospace engineering.en
dc.subjectMajor aerospace engineering.en
dc.titleStudy of active control of instability in a boundary layer over a flat plate flowen
dc.typeThesisen
thesis.degree.disciplineaerospace engineeringen
thesis.degree.nameM.S.en
thesis.degree.levelMastersen
dc.type.genrethesisen
dc.type.materialtexten
dc.format.digitalOriginreformatted digitalen


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