Reynolds number effects on the unsteady aerodynamic behavior of an NACA 0012 airfoil
Name
15608098-MIT.pdf
Size
28.2 MB
Format
Adobe PDF
Checksum (MD5)
a00f13eea13e87b113fcaa5cdacc22cf
Author(s)
Fletcher, Michael Joseph.
Advisor(s)
Eugene E. Covert.
Date Issued
1986
Publisher
Massachusetts Institute of Technology
Description
Thesis: M.S., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 1986
Bibliography: leaves 93-95.
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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