An experimental low Reynolds number comparison of a Wortmann FX67-K170 airfoil, a NACA 0012 airfoil, and a NACA 64-210 airfoil in simulated heavy rain
Name
16262992-MIT.pdf
Size
21.02 MB
Format
Adobe PDF
Checksum (MD5)
084158453e23c1d1b6dba4eecce89202
Author(s)
Craig, Anthony Paul.
Advisor(s)
R. John Hansman.
Date Issued
1987
Publisher
Massachusetts Institute of Technology
Description
Thesis: M.S., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 1987
Bibliography: leaves 102-103.
Subjects
Aeronautics and Astronautics.
MIT Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Terms of Use
MIT theses may be protected by copyright. Please reuse MIT thesis content according to the MIT Libraries Permissions Policy, which is available through the URL provided.
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