The effects of trailing edge bluntness on airfoil performance as calculated approximately by a viscid-inviscid vortex panel method
Name
20404644-MIT.pdf
Description
Full printable version
Size
4.02 MB
Format
Adobe PDF
Checksum (MD5)
9fc5b182159b0ab4414e1ed9d3b583d3
Author(s)
D'Angelo, Michael R. (Michael Ronald)
Advisor(s)
Eugene E. Covert.
Date Issued
1989
Publisher
Massachusetts Institute of Technology
Description
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989.
Includes bibliographical references (leaves 86-88).
Subjects
Aeronautics and Astronautics.
MIT Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Terms of Use
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