Aerodynamic characteristics of the NACA 8-H-12 airfoil section at six Reynolds numbers from 1.8 x 10⁶ to 11.0 x 10⁶ /
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Author / Creator: | Schaefer, Raymond F., author. |
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Imprint: | Washington, [D.C.] : National Advisory Committee for Aeronautics, 1949. |
Description: | 1 online resource (12 pages) : illustrations. |
Language: | English |
Series: | Technical notes / National Advisory Committee for Aeronautics ; No. 1998 Technical note (United States. National Advisory Committee for Aeronautics) ; 1998. |
Subject: | |
Format: | E-Resource U.S. Federal Government Document Book |
URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/12346604 |
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086 | 0 | |a Y 3.N 21/5:6/1998 | |
100 | 1 | |a Schaefer, Raymond F., |e author. | |
245 | 1 | 0 | |a Aerodynamic characteristics of the NACA 8-H-12 airfoil section at six Reynolds numbers from 1.8 x 10⁶ to 11.0 x 10⁶ / |c by Raymond F. Schaefer and Hamilton A. Smith. |
246 | 3 | |a Aerodynamic characteristics of the National Advisory Committee for Aeronautics 8-H-12 airfoil section at six Reynolds numbers from 1.8 x 10(exp 6) to 11.0 x 10(exp 6) | |
264 | 1 | |a Washington, [D.C.] : |b National Advisory Committee for Aeronautics, |c 1949. | |
300 | |a 1 online resource (12 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. 1998 | |
588 | |a Description based on online resource, PDF version; title from title page (TRAIL, viewed July 9, 2020). | ||
500 | |a "December 1949." | ||
500 | |a No Federal Depository Library Program (FDLP) item number. | ||
504 | |a Includes bibliographical references (page 8). | ||
650 | 0 | |a Aerofoils. |0 http://id.loc.gov/authorities/subjects/sh85001301 | |
650 | 0 | |a Aerodynamics. |0 http://id.loc.gov/authorities/subjects/sh85001295 | |
650 | 0 | |a Lift (Aerodynamics) |0 http://id.loc.gov/authorities/subjects/sh85076855 | |
650 | 0 | |a Drag (Aerodynamics) |0 http://id.loc.gov/authorities/subjects/sh85039270 | |
650 | 0 | |a Pitching (Aerodynamics) |0 http://id.loc.gov/authorities/subjects/sh85102496 | |
650 | 0 | |a Wind tunnel testing. |0 http://id.loc.gov/authorities/subjects/sh2007008292 | |
650 | 7 | |a Aerodynamics. |2 fast |0 (OCoLC)fst00798195 | |
650 | 7 | |a Aerofoils. |2 fast |0 (OCoLC)fst00798241 | |
650 | 7 | |a Drag (Aerodynamics) |2 fast |0 (OCoLC)fst00897351 | |
650 | 7 | |a Lift (Aerodynamics) |2 fast |0 (OCoLC)fst00998431 | |
650 | 7 | |a Pitching (Aerodynamics) |2 fast |0 (OCoLC)fst01064896 | |
650 | 7 | |a Wind tunnel testing. |2 fast |0 (OCoLC)fst01744047 | |
700 | 1 | |a Smith, Hamilton A., |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 Schaefer, Raymond F., |t Aerodynamic characteristics of the NACA 8-H-12 airfoil section at six Reynolds numbers from 1.8 x 10(exp 6) to 11.0 x 10(exp 6) |w (OCoLC)662479568 |
830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v 1998. | |
856 | 4 | 0 | |u https://purl.fdlp.gov/GPO/gpo141161 |y Government Publishing Office |
903 | |a HeVa | ||
929 | |a eresource | ||
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