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dc.contributor.advisorHealey, J. Val
dc.contributor.authorNarveson, Marshall L.
dc.date1990-09
dc.date.accessioned2013-08-01T21:15:49Z
dc.date.available2013-08-01T21:15:49Z
dc.date.issued1990-09
dc.identifier.urihttps://hdl.handle.net/10945/34915
dc.description.abstractThe Naval Postgraduate School (NPS) has undertaken a series of studies on ship air wake tailoring, through the use of deflectors, with the goal of reducing the level of turbulence and the size of the separated zones on the helicopter deck. This reduction will result in a larger engagedisengage envelope, which in turn, will increase the percentage of time that the H-46 and other helicopters can safely operate. This study is the second in the series of NPS to attempt to achieve this goal and considers only the feasibility of tailoring a two-dimensional flow over a backward facing step. Nonporous flat and curved deflectors and porous flat deflectors were mounted in various positions near the edge of the step and the flow patterns recorded using both still and video photography. The deflectors were mounted at varying separations from the step and varying angles to the vertical. It was found that the porous deflectors produced the lowest velocities in the region behind the step, and the nonporous produced the greatest changes in the flow pattern. The results were also compared to the results of the first study that used the 'PHOENICS' computational fluid dynamics program. With one exception, the results differed only by the underprediction of the length of the horizontal flow pattern.en_US
dc.description.urihttp://archive.org/details/flowmodification1094534915
dc.format.extentxii, 87 p. ill.en_US
dc.languageen_US
dc.publisherMonterey, California: Naval Postgraduate Schoolen_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.en_US
dc.subject.lcshEngineeringen_US
dc.subject.lcshAerodynamicsen_US
dc.subject.lcshMarine engineering.en_US
dc.titleFlow modification over a backward facing stepen_US
dc.typeThesisen_US
dc.contributor.secondreaderHoward, Richard M.
dc.contributor.corporateNaval Postgraduate School (U.S.)
dc.contributor.departmentAeronautics and Astronautics
dc.subject.authorBackward Facing Stepen_US
dc.subject.authorFlow Visualizationen_US
dc.subject.authorBluff Body Aerodynamicsen_US
dc.subject.authorHelium Bubble Flow Visualizationen_US
dc.subject.authorDeflectorsen_US
dc.subject.authorFlow Modificationen_US
dc.description.serviceLieutenant Commander, United States Navyen_US
etd.thesisdegree.nameM.S. in Aeronautical Engineeringen_US
etd.thesisdegree.levelMastersen_US
etd.thesisdegree.disciplineAeronautical Engineeringen_US
etd.thesisdegree.grantorNaval Postgraduate Schoolen_US
dc.description.distributionstatementApproved for public release; distribution is unlimited.


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