| dc.contributor.author | Craig, Anthony Paul. | en_US |
| dc.contributor.other | Massachusetts Institute of Technology. Department of Aeronautics and Astronautics. | en_US |
| dc.date.accessioned | 2023-04-21T20:19:08Z | |
| dc.date.available | 2023-04-21T20:19:08Z | |
| dc.date.copyright | 1987 | en_US |
| dc.date.issued | 1987 | en_US |
| dc.identifier.uri | https://hdl.handle.net/1721.1/150505 | |
| dc.description | Thesis: M.S., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 1987 | en_US |
| dc.description | Bibliography: leaves 102-103. | en_US |
| dc.description.statementofresponsibility | by Anthony Paul Craig. | en_US |
| dc.format.extent | 106 leaves | en_US |
| dc.publisher | Massachusetts Institute of Technology | en_US |
| dc.rights | 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. | en_US |
| dc.rights.uri | http://dspace.mit.edu/handle/1721.1/7582 | en_US |
| dc.subject | Aeronautics and Astronautics. | en_US |
| dc.title | 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 | en_US |
| dc.type | Thesis | en_US |
| dc.description.degree | M.S. | en_US |
| dc.contributor.department | Massachusetts Institute of Technology. Department of Aeronautics and Astronautics | en_US |
| dc.identifier.oclc | 16262992 | en_US |
| dc.description.collection | M.S. Massachusetts Institute of Technology, Department of Aeronautics and Astronautics | en_US |
| dspace.imported | 2023-04-21T20:19:08Z | en_US |
| mit.thesis.degree | Master | en_US |
