Wind tunnel pressure distribution tests on a series of biplane wing models. Part II. Effects of changes in decalage, dihedral, sweepback and overhang /
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| Author / Creator: | Knight, Montgomery, author. |
|---|---|
| Imprint: | Washington, [D.C.] : National Advisory Committee for Aeronautics, 1929. |
| Description: | 1 online resource (6 pages, 32 unnumbered pages) : illustrations. |
| Language: | English |
| Series: | Technical notes / National Advisory Committee for Aeronautics ; No. 325 Technical note (United States. National Advisory Committee for Aeronautics) ; 325. |
| Subject: | |
| Format: | E-Resource U.S. Federal Government Document Book |
| URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/12553704 |
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| 100 | 1 | |a Knight, Montgomery, |e author. |0 http://id.loc.gov/authorities/names/no2020121090 |1 http://viaf.org/viaf/3155160364974563680002 | |
| 245 | 1 | 0 | |a Wind tunnel pressure distribution tests on a series of biplane wing models. |n Part II. |p Effects of changes in decalage, dihedral, sweepback and overhang / |c by Montgomery Knight and Richard W. Noyes. |
| 246 | 3 | 0 | |a Effects of changes in decalage, dihedral, sweepback and overhang |
| 264 | 1 | |a Washington, [D.C.] : |b National Advisory Committee for Aeronautics, |c 1929. | |
| 300 | |a 1 online resource (6 pages, 32 unnumbered pages) : |b illustrations. | ||
| 336 | |a text |b txt |2 rdacontent |0 http://id.loc.gov/vocabulary/contentTypes/txt | ||
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| 490 | 1 | |a Technical notes / National Advisory Committee for Aeronautics ; |v No. 325 | |
| 588 | |a Description based on online resource, PDF version; title from title page (TRAIL, viewed August 31, 2020). | ||
| 500 | |a "October, 1929." | ||
| 500 | |a Includes errata. | ||
| 500 | |a No Federal Depository Library Program (FDLP) item number. | ||
| 504 | |a Includes bibliographical reference (page 6). | ||
| 650 | 0 | |a Airplanes |x Dihedral wings. |0 http://id.loc.gov/authorities/subjects/sh2002010118 | |
| 650 | 0 | |a Airplanes |x Models |x Testing. | |
| 650 | 0 | |a Airplanes |x Wings, Swept-back. |0 http://id.loc.gov/authorities/subjects/sh85002928 | |
| 650 | 0 | |a Aerodynamic load |x Testing. | |
| 650 | 0 | |a Wind tunnel testing. |0 http://id.loc.gov/authorities/subjects/sh2007008292 | |
| 650 | 0 | |a Biplanes. |0 http://id.loc.gov/authorities/subjects/sh85014272 | |
| 650 | 7 | |a Aerodynamic load |x Testing. |2 fast |0 (OCoLC)fst00798185 | |
| 650 | 7 | |a Airplanes |x Dihedral wings. |2 fast |0 (OCoLC)fst00803147 | |
| 650 | 7 | |a Airplanes |x Models |x Testing. |2 fast |0 (OCoLC)fst00803318 | |
| 650 | 7 | |a Airplanes |x Wings, Swept-back. |2 fast |0 (OCoLC)fst00803560 | |
| 650 | 7 | |a Wind tunnel testing. |2 fast |0 (OCoLC)fst01744047 | |
| 700 | 1 | |a Noyes, Richard W., |e author. |0 http://id.loc.gov/authorities/names/no2020121086 |1 http://viaf.org/viaf/14160362833263502950 | |
| 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 Knight, Montgomery |t Wind tunnel pressure distribution tests on a series of biplane wing models. Part II, Effects of changes in decalage, dihedral, sweepback and overhang |w (OCoLC)642700099 |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v 325. | |
| 856 | 4 | 0 | |u https://purl.fdlp.gov/GPO/gpo144234 |y Government Publishing Office |
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