Contributions to the analysis of high-lift airfoil aerodynamics.
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Authors
Lee, Hee Woo
Subjects
computational analysis of inviscid, viscous and interaction schemes
Advisors
Platzer, M.F.
Date of Issue
1986-03
Date
March 1986
Publisher
Language
en_US
Abstract
This thesis treats the problem of incompressible two-dimensional
steady flow past airfoils or airfoil combinations
at large angles of attack. A panel method was developed to
compute the inviscid flow over two cylinders, airfoil-flap
combinations and airfoils in ground effect. In addition,
Cebeci's viscous/inviscid interaction method was applied to
several airfoils and compared with available experimental
data. The agreement is generally quite encouraging.
Type
Thesis
Description
Series/Report No
Department
Aeronautics
Organization
Naval Postgraduate School (U.S.)
Identifiers
NPS Report Number
Sponsors
Funder
Format
101 p.
Citation
Distribution Statement
Approved for public release; distribution is unlimited.
Rights
Copyright is reserved by the copyright owner