Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/45845
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dc.contributor.authorTeo, Wilson Seng Kee.-
dc.date.accessioned2011-06-22T06:21:03Z-
dc.date.available2011-06-22T06:21:03Z-
dc.date.copyright2011en_US
dc.date.issued2011-
dc.identifier.urihttp://hdl.handle.net/10356/45845-
dc.description.abstractSynthetic jet actuators (SJA) are a new class of flow control devices that can be used to increase the momentum of flow over the surface by injecting a massless jet (without any additional air supply) for effective delay of flow separation. It consists of a walled cavity enclosed with an orifice plate at one end and an oscillating diaphragm at the other, creating a successive vortex ring. The vortex ring is developed due to differences in velocity at the orifice during a push-stroke of the diaphragm.en_US
dc.format.extent104 p.en_US
dc.language.isoenen_US
dc.rightsNanyang Technological University-
dc.subjectDRNTU::Engineering::Aeronautical engineering::Aerodynamicsen_US
dc.titleAn experimental study of synthetic jetsen_US
dc.typeFinal Year Project (FYP)en_US
dc.contributor.schoolSchool of Mechanical and Aerospace Engineeringen_US
dc.description.degreeBachelor of Engineering (Mechanical Engineering)en_US
dc.contributor.supervisor2Tang Huien_US
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Appears in Collections:MAE Student Reports (FYP/IA/PA/PI)
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