Aerodynamic characteristics of the NACA 64-010 and 0010-1.10 40/1.051 airfoil sections at Mach numbers from 0.30 to 0.85 and Reynolds numbers from 4.0 x 10⁶ to 8.0 x 10⁶ /
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| Author / Creator: | Loftin, Laurence K., author. |
|---|---|
| Imprint: | Washington, [D.C.] : National Advisory Committee for Aeronautics, 1954. |
| Description: | 1 online resource (17 pages) : illustrations. |
| Language: | English |
| Series: | Technical notes / National Advisory Committee for Aeronautics ; No. 3244 Technical note (United States. National Advisory Committee for Aeronautics) ; 3244. |
| Subject: | |
| Format: | E-Resource U.S. Federal Government Document Book |
| URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/12381209 |
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| 100 | 1 | |a Loftin, Laurence K., |e author. |0 http://id.loc.gov/authorities/names/n81102921 |1 http://viaf.org/viaf/15079613 | |
| 245 | 1 | 0 | |a Aerodynamic characteristics of the NACA 64-010 and 0010-1.10 40/1.051 airfoil sections at Mach numbers from 0.30 to 0.85 and Reynolds numbers from 4.0 x 10⁶ to 8.0 x 10⁶ / |c by Laurence K. Loftin, Jr. |
| 246 | 3 | |a Aerodynamic characteristics of the National Advisory Committee for Aeronautics 64-010 and 0010-1.10 40/1.051 airfoil sections at Mach numbers from 0.30 to 0.85 and Reynolds numbers from 4.0 x 10(exp. 6) to 8.0 x 10(exp. 6) | |
| 264 | 1 | |a Washington, [D.C.] : |b National Advisory Committee for Aeronautics, |c 1954. | |
| 300 | |a 1 online resource (17 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 | ||
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| 490 | 1 | |a Technical notes / National Advisory Committee for Aeronautics ; |v No. 3244 | |
| 588 | |a Description based on online resource, PDF version; title from title page (TRAIL, viewed August 7, 2020). | ||
| 500 | |a "August 1954." | ||
| 500 | |a No Federal Depository Library Program (FDLP) item number. | ||
| 504 | |a Includes bibliographical references (page 5). | ||
| 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 Mach number. |0 http://id.loc.gov/authorities/subjects/sh85079305 | |
| 650 | 0 | |a Reynolds number. |0 http://id.loc.gov/authorities/subjects/sh85113557 | |
| 650 | 7 | |a Aerodynamics. |2 fast |0 (OCoLC)fst00798195 | |
| 650 | 7 | |a Aerofoils. |2 fast |0 (OCoLC)fst00798241 | |
| 650 | 7 | |a Mach number. |2 fast |0 (OCoLC)fst01004756 | |
| 650 | 7 | |a Reynolds number. |2 fast |0 (OCoLC)fst01096833 | |
| 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 Loftin, Laurence K., |t Aerodynamic characteristics of the NACA 64-010 and 0010-1.10 40/1.051 airfoil sections at Mach numbers from 0.30 to 0.85 and Reynolds numbers from 4.0 x 10(exp. 6) to 8.0 x 10(exp. 6) |w (OCoLC)671756527 |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v 3244. | |
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