Aerodynamic characteristics of a circular cylinder at Mach number 6.86 and angles of attack up to 90° /
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| Author / Creator: | Penland, Jim A., author. |
|---|---|
| Imprint: | Washington, [D.C.] : National Advisory Committee for Aeronautics, 1957. |
| Description: | 1 online resource (32 pages) : illustrations. |
| Language: | English |
| Series: | Technical notes / National Advisory Committee for Aeronautics ; No. 3861 Technical note (United States. National Advisory Committee for Aeronautics) ; 3861. |
| Subject: | |
| Format: | E-Resource U.S. Federal Government Document Book |
| URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/12381204 |
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| 100 | 1 | |a Penland, Jim A., |e author. |0 http://id.loc.gov/authorities/names/n79015944 |1 http://viaf.org/viaf/20954167 | |
| 245 | 1 | 0 | |a Aerodynamic characteristics of a circular cylinder at Mach number 6.86 and angles of attack up to 90° / |c by Jim A. Penland. |
| 246 | 3 | |a Aerodynamic characteristics of a circular cylinder at Mach number 6.86 and angles of attack up to ninety degrees | |
| 264 | 1 | |a Washington, [D.C.] : |b National Advisory Committee for Aeronautics, |c 1957. | |
| 300 | |a 1 online resource (32 pages) : |b illustrations. | ||
| 336 | |a text |b txt |2 rdacontent |0 http://id.loc.gov/vocabulary/contentTypes/txt | ||
| 337 | |a computer |b c |2 rdamedia |0 http://id.loc.gov/vocabulary/mediaTypes/c | ||
| 338 | |a online resource |b cr |2 rdacarrier |0 http://id.loc.gov/vocabulary/carriers/cr | ||
| 490 | 1 | |a Technical notes / National Advisory Committee for Aeronautics ; |v No. 3861 | |
| 588 | |a Description based on online resource, PDF version; title from title page (TRAIL, viewed August 13, 2020). | ||
| 500 | |a "January 1957." | ||
| 500 | |a "Supersedes recently declassified NACA Research Memorandum L54A14 by Jim A. Penland, 1954"--Page 1. | ||
| 500 | |a No Federal Depository Library Program (FDLP) item number. | ||
| 504 | |a Includes bibliographical references (page 13-14). | ||
| 650 | 0 | |a Cylinders |x Aerodynamics. |0 http://id.loc.gov/authorities/subjects/sh2003003315 | |
| 650 | 0 | |a Aerodynamic load. |0 http://id.loc.gov/authorities/subjects/sh85001292 | |
| 650 | 0 | |a Wind tunnel testing. |0 http://id.loc.gov/authorities/subjects/sh2007008292 | |
| 650 | 0 | |a Hypersonic wind tunnels. |0 http://id.loc.gov/authorities/subjects/sh85063719 | |
| 650 | 7 | |a Aerodynamic load. |2 fast |0 (OCoLC)fst00798180 | |
| 650 | 7 | |a Cylinders |x Aerodynamics. |2 fast |0 (OCoLC)fst00886042 | |
| 650 | 7 | |a Hypersonic wind tunnels. |2 fast |0 (OCoLC)fst00965824 | |
| 650 | 7 | |a Wind tunnel testing. |2 fast |0 (OCoLC)fst01744047 | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics, |e issuing body. |0 http://id.loc.gov/authorities/names/n79060141 |1 http://viaf.org/viaf/136563305 | |
| 776 | 0 | 8 | |i Print version: |a Penland, Jim A., |t Aerodynamic characteristics of a circular cylinder at Mach number 6.86 and angles of attack up to 90 degrees |w (OCoLC)686744106 |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v 3861. | |
| 856 | 4 | 0 | |u https://purl.fdlp.gov/GPO/gpo143051 |y Government Publishing Office |
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| 928 | |t Library of Congress classification |l Online |c UC-FullText |u https://purl.fdlp.gov/GPO/gpo143051 |z Government Publishing Office |g ebooks |i 11981315 | ||