Wind tunnel pressure distribution tests on an airfoil with trailing edge flap /
Saved in:
| Author / Creator: | Wenzinger, Carl J. (Carl Joseph), 1903-1988, author. |
|---|---|
| Imprint: | Washington, [D.C.] : National Advisory Committee for Aeronautics, 1929. |
| Description: | 1 online resource (10 pages, 12 unnumbered pages) : illustrations. |
| Language: | English |
| Series: | Technical notes / National Advisory Committee for Aeronautics ; No. 326 Technical note (United States. National Advisory Committee for Aeronautics) ; 326. |
| Subject: | |
| Format: | E-Resource U.S. Federal Government Document Book |
| URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/12553696 |
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| 100 | 1 | |a Wenzinger, Carl J. |q (Carl Joseph), |d 1903-1988, |e author. |0 http://id.loc.gov/authorities/names/n2011083130 |1 http://viaf.org/viaf/221120102 | |
| 245 | 1 | 0 | |a Wind tunnel pressure distribution tests on an airfoil with trailing edge flap / |c by Carl J. Wenzinger and Oscar Loeser, Jr. |
| 264 | 1 | |a Washington, [D.C.] : |b National Advisory Committee for Aeronautics, |c 1929. | |
| 300 | |a 1 online resource (10 pages, 12 unnumbered 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. 326 | |
| 588 | |a Description based on online resource, PDF version; title from title page (TRAIL, viewed August 31, 2020). | ||
| 500 | |a "October, 1929." | ||
| 500 | |a No Federal Depository Library Program (FDLP) item number. | ||
| 504 | |a Includes bibliographical references (pages 7-8). | ||
| 650 | 0 | |a Aerofoils. |0 http://id.loc.gov/authorities/subjects/sh85001301 | |
| 650 | 0 | |a Flaps (Airplanes) |0 http://id.loc.gov/authorities/subjects/sh85049001 | |
| 650 | 0 | |a Wind tunnel testing. |0 http://id.loc.gov/authorities/subjects/sh2007008292 | |
| 650 | 0 | |a Aerodynamic load |x Testing. | |
| 650 | 7 | |a Aerodynamic load |x Testing. |2 fast |0 (OCoLC)fst00798185 | |
| 650 | 7 | |a Wind tunnel testing. |2 fast |0 (OCoLC)fst01744047 | |
| 700 | 1 | |a Loeser, Oscar, |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 Print version: |a Wenzinger, Carl J. |t Wind tunnel pressure distribution tests on an airfoil with trailing edge flap |w (OCoLC)642704145 |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v 326. | |
| 856 | 4 | 0 | |u https://purl.fdlp.gov/GPO/gpo144235 |y Government Publishing Office |
| 903 | |a HeVa | ||
| 929 | |a eresource | ||
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| 928 | |t Library of Congress classification |l Online |c UC-FullText |u https://purl.fdlp.gov/GPO/gpo144235 |z Government Publishing Office |g ebooks |i 12330907 | ||