An analytical model for highly separated flow on airfoils at low speeds
Zumwalt, Glen Wallace, 1926-2011 Naik, Sharad N.
Zumwalt, Glen Wallace, 1926-2011
Naik, Sharad N.
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Location
Time Period
Advisors
Original Date
Digitization Date
Issue Date
1977
Type
Book
Genre
Keywords
Aerofoils,Air flow,Boundary layer
Subjects (LCSH)
Citation
Glen 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.
Abstract
A 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.
Table of Contents
Description
Consists 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
Final report to National Aeronautics and Space Administration, Langley Research Center, Hampton, Virginia. Grant NSG 1192.
Final report to National Aeronautics and Space Administration, Langley Research Center, Hampton, Virginia. Grant NSG 1192.
Publisher
Department of Aeronautical Engineering, Wichita State University
Journal
Book Title
Series
Aeronautical report (Wichita State University. Aeronautical Engineering Department) ;AR 77-2.