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 |
Item Description: | Prepared for contract no. AF 18 (600)-1523. AFOSR TN56-532, TN57-68; ASTIA no. AD110351, AD-120-410. |
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Physical Description: | v. |