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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

Author(s)
Craig, Anthony Paul.
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Massachusetts Institute of Technology. Department of Aeronautics and Astronautics.
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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. http://dspace.mit.edu/handle/1721.1/7582
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Description
Thesis: M.S., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 1987
 
Bibliography: leaves 102-103.
 
Date issued
1987
URI
https://hdl.handle.net/1721.1/150505
Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Publisher
Massachusetts Institute of Technology
Keywords
Aeronautics and Astronautics.

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