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dc.contributor.authorToebes, G. H.en_US
dc.contributor.authorPerkins, F. E.en_US
dc.contributor.authorEagleson, P. S.en_US
dc.date.accessioned2022-06-13T13:12:09Z
dc.date.available2022-06-13T13:12:09Z
dc.date.issued1958-04
dc.identifier3
dc.identifier.urihttps://hdl.handle.net/1721.1/143046
dc.descriptionPrepared under David Taylor Model Basin, U.S. Dept. of the Navy Nonr-1841(21)en_US
dc.description.abstractThis Technical Note describes the design of an open-circuit water tunnel with a 7-1/2 inch by 9 inch closed-jet working section. The maximum velocity obtainable in the empty test section is approximately 50 fps. The water tunnel was built for the purpose of investigating wakes behind objects placed in its test section. In particular, a study is to be made of the relationship between the trailing edge geometry of two-dimensional flat plates, the frequency of vortex shedding from them and the resulting elastic response of the plates when placed at zero angle of attack.en_US
dc.publisherCambridge, Mass. : Hydrodynamics Laboratory, Dept. of Civil and Sanitary Engineering, Massachusetts Institute of Technology
dc.relation.ispartofseriesTechnical note (Massachusetts Institute of Technology. Hydrodynamics Laboratory) ; no. 3.
dc.titleDesign of a Closed Jet, Open Circuit Water Tunnel for the Study of Wake Mechanicsen_US
dc.identifier.oclc13825031
dc.identifier.aleph245552


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