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dc.contributor.authorZumwalt, Glen Wallace,1926-2011
dc.contributor.authorNaik, Sharad N.
dc.date.accessioned2017-12-01T21:19:11Z
dc.date.available2017-12-01T21:19:11Z
dc.date.issued1977
dc.identifier.citationGlen W. Zumwalt and Sharad N. Naik, An analytical model for highly separated flow on airfoils at low speeds (Wichita, KS: Department of Aeronautical Engineering, Wichita State University, 1977), 106 leaves.
dc.identifier.other353385
dc.identifier.urihttp://hdl.handle.net/10057/14367
dc.descriptionConsists largely of Sharad N. Naik's doctoral dissertation at Wichita State University/[University of Kansas] carried out under the guidance of Prof. Glen W. Zumwalt
dc.descriptionFinal report to National Aeronautics and Space Administration, Langley Research Center, Hampton, Virginia. Grant NSG 1192.
dc.description.abstractA computer program has been developed to solve the low speed flow around airfoils with highly separated flow. A new flow model, which was suggested by Zumwalt , included all of the major physical features in the separated region. It was suggested by experimental airfoil studies made in the WSU low speed wind tunnel. Flow visualization tests also were made which gave substantiation to the validity of the model. The computation involves the matching of the potential flow, boundary layer and flows in the separated regions.
dc.format.extent106 leaves: ill. ;28 cm.
dc.language.isoen_us
dc.publisherDepartment of Aeronautical Engineering, Wichita State University
dc.relation.ispartofseriesAeronautical report (Wichita State University. Aeronautical Engineering Department) ;AR 77-2.
dc.subjectAerofoils
dc.subjectAir flow
dc.subjectBoundary layer
dc.subject.lccTL501.W5 AR 77-2
dc.titleAn analytical model for highly separated flow on airfoils at low speeds
dc.title.alternativeSeparated flow on low speed airfoils
dc.typeTechnical report


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