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: | Aerodynamics, Supersonic. Laminar boundary layer. |
Format: | Print Book |
URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/4134946 |
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001 | 4134946 | ||
003 | ICU | ||
005 | 20000113000000.0 | ||
008 | 991102m19569999nyu 000 0 eng d | ||
035 | |a (OCoLC)237188482 | ||
040 | |a CGU |c CGU | ||
049 | |a CGUA | ||
110 | 2 | |a Cornell University. |b Graduate School of Aeronautical Engineering. | |
245 | 1 | 0 | |a Laminar boundary layer on a spinning circular cone in supersonic flow at a small angle of attack, |c by Martin Fiebig. |
260 | |a Ithaca, N.Y., |c 1956- | ||
300 | |a v. | ||
336 | |a text |b txt |2 rdacontent | ||
337 | |a unmediated |b n |2 rdamedia | ||
338 | |a volume |b nc |2 rdacarrier | ||
500 | |a Prepared for contract no. AF 18 (600)-1523. | ||
500 | |a AFOSR TN56-532, TN57-68; ASTIA no. AD110351, AD-120-410. | ||
650 | 7 | |a Aerodynamics, Supersonic. |2 fast |0 http://id.worldcat.org/fast/fst00798221 | |
650 | 7 | |a Laminar boundary layer. |2 fast |0 http://id.worldcat.org/fast/fst00991078 | |
700 | 1 | |a Fiebig, Martin. | |
710 | 1 | |a United States. |b Air Force. |b Office of Scientific Research. |b Mechanics Division | |
903 | |a Hathi | ||
929 | |a retrocon | ||
999 | f | f | |i b2929356-d823-5be8-b732-6c52dde827e8 |s b17c207e-1547-5c00-814b-03f2327d6291 |
928 | |t Dewey Decimal classification |a TE3a 628 |l JCL |c JCL-SciDDC |i 477240 | ||
927 | |t Dewey Decimal classification |a TE3a 628 |v 1956 Jun |l JCL |c JCL-SciDDC |e CRERAR |b 105162646 |i 6606663 | ||
927 | |t Dewey Decimal classification |a TE3a 628 |v 1957 Feb |l JCL |c JCL-SciDDC |e CRERAR |b 105162581 |i 6606664 |