Theses and Dissertations
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Contributions to the analysis of high-lift airfoil aerodynamics.
(1986-03)
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, ...
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Advisor
Author
Branch Of Service
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Captain, Korea Air Force (1)
Date Issued
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1986 (1)
Degree
Department
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Aeronautical Engineering (1)