Laminar boundary layer on a spinning circular cone in supersonic flow at a small angle of attack,
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| Corporate author / creator: | Cornell University. Graduate School of Aeronautical Engineering. |
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| Imprint: | Ithaca, N.Y., 1956- |
| Description: | v. |
| Language: | English |
| Subject: | |
| Format: | Print Book |
| URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/4134946 |
