Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0° to 20° at high subsonic speeds /
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| Author / Creator: | Daley, Bernard N., author. |
|---|---|
| Imprint: | Washington, [D.C.] : National Advisory Committee for Aeronautics, 1955. |
| Description: | 1 online resource (57 pages) : illustrations. |
| Language: | English |
| Series: | Technical notes / National Advisory Committee for Aeronautics ; No. 3424 Technical note (United States. National Advisory Committee for Aeronautics) ; 3424. |
| Subject: | |
| Format: | E-Resource U.S. Federal Government Document Book |
| URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/12381208 |
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| 100 | 1 | |a Daley, Bernard N., |e author. | |
| 245 | 1 | 0 | |a Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0° to 20° at high subsonic speeds / |c by Bernard N. Daley and Douglas R. Lord. |
| 246 | 3 | |a Aerodynamic characteristics of several six-percent-thick airfoils at angles of attack from zero degrees to twenty degrees at high subsonic speeds | |
| 264 | 1 | |a Washington, [D.C.] : |b National Advisory Committee for Aeronautics, |c 1955. | |
| 300 | |a 1 online resource (57 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. 3424 | |
| 588 | |a Description based on online resource, PDF version; title from title page (TRAIL, viewed August 11, 2020). | ||
| 500 | |a "May 1955." | ||
| 500 | |a "Supersedes recently declassified NACA RM L9E19. 1949"--Page 1. | ||
| 500 | |a No Federal Depository Library Program (FDLP) item number. | ||
| 504 | |a Includes bibliographical references (page 10). | ||
| 650 | 0 | |a Aerofoils |x Testing. | |
| 650 | 0 | |a Angle of attack (Aerodynamics) |0 http://id.loc.gov/authorities/subjects/sh95010977 | |
| 650 | 7 | |a Aerofoils |x Testing. |2 fast |0 (OCoLC)fst00798250 | |
| 650 | 7 | |a Angle of attack (Aerodynamics) |2 fast |0 (OCoLC)fst00808866 | |
| 700 | 1 | |a Lord, Douglas T., |e author. | |
| 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 Paper version: |a Daley, Bernard N., |t Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0 to 20 degrees at high subsonic speeds |w (OCoLC)679716891 |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v 3424. | |
| 856 | 4 | 0 | |u https://purl.fdlp.gov/GPO/gpo142885 |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/gpo142885 |z Government Publishing Office |g ebooks |i 11981319 | ||