Upstream effects of secondary injection on the profiles of a boundary layer over a flat plate.

dc.contributor.authorHofford, Robert Francis.
dc.contributor.corporateStanford University
dc.contributor.departmentAeronautics and Astronautics
dc.dateSeptember 1971
dc.date.accessioned2012-11-13T23:25:45Z
dc.date.available2012-11-13T23:25:45Z
dc.date.issued1971-09
dc.descriptionThis thesis document was issued under the authority of another institution, not NPS. At the time it was written, a copy was added to the NPS Library Collection for reasons not now known. It has been included in the digital archive for its historical value to NPS. Not believed to be a CIVINS (Civilian Institutions) title.
dc.description.abstractAn account is given of the effect on the boundary layer of a secondary air flow directed normal to a flat plate immersed in a primary flow field of uniform velocity. System design and tunnel operation are discussed briefly. Boundary layer profiles are compared to existing theory and secondary injection effects are discussed. The work described in this thesis was initiated by the author following exposure to the field of jet interaction. Boundary layer conditions during portions of flight where the airstream is subsonic and jet interaction is the means of control posed the problem considered herein.
dc.description.serviceLieutenant Commander, United States Navy
dc.description.urihttp://archive.org/details/upstreameffectso1094515955
dc.identifier.urihttps://hdl.handle.net/10945/15955
dc.language.isoen_US
dc.publisherStanford Universityen_US
dc.rightsThis publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.
dc.subject.lcshAeronauticsen_US
dc.titleUpstream effects of secondary injection on the profiles of a boundary layer over a flat plate.en_US
dc.typeThesisen_US
dspace.entity.typePublication
etd.thesisdegree.disciplineEngineeringen_US
etd.thesisdegree.grantorStanford Universityen_US
etd.thesisdegree.levelProfessional Degreeen_US
etd.thesisdegree.nameDegree of engineeren_US
Files
Original bundle
Now showing 1 - 1 of 1
Loading...
Thumbnail Image
Name:
upstreameffectso00hoff.pdf
Size:
1.21 MB
Format:
Adobe Portable Document Format
Collections