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dc.creatorOlson, Milford Eugene
dc.date.accessioned2012-06-07T16:35:50Z
dc.date.available2012-06-07T16:35:50Z
dc.date.created1967
dc.date.issued1967
dc.identifier.urihttps://hdl.handle.net/1969.1/ETD-TAMU-1967-THESIS-O52
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.description.abstractMany methods for the control of boundary layer separation are currently being used. These include the control of body shape, smoothness, suction, slots, slats, or the use of a tangential blowing air jet. Other suggested methods are the undulation or movement of body surfaces. However, the least understood of the methods is probably that of the tangential blowing air jet, even though research has indicated that the addition of mass by tangential blowing has a substantial effect on delaying flow separation over airfoils.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.titleThe effect of tangential blowing on boundary-layer profilesen
dc.typeThesisen
thesis.degree.disciplineaerospace engineeringen
thesis.degree.nameM.S. in Aerospace Engineeringen
thesis.degree.levelMastersen
dc.type.genrethesisen
dc.type.materialtexten
dc.format.digitalOriginreformatted digitalen


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