Implementation of a separated flow panel method for wall effects on finite swept wings

Robinson, Donald Edwin

Implementation of a separated flow panel method for wall effects on finite swept wings

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20054849-MIT.pdf

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Author(s)

Robinson, Donald Edwin

Advisor(s)

Judson R. Baron.

Date Issued

1988

Publisher

Massachusetts Institute of Technology

Description

Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.

Includes bibliographical references.

Subjects

Aeronautics and Astronautics.

MIT Department

Massachusetts Institute of Technology. Department of Aeronautics and Astronautics

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http://dspace.mit.edu/handle/1721.1/7582

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http://hdl.handle.net/1721.1/35342