Effect of shape changes on the aerodynamic characteristics of a twisted and cambered arrow wing at Mach number 2.03 /
Saved in:
| Author / Creator: | Landrum, Emma Jean, author. |
|---|---|
| Imprint: | Washington, D.C. : National Aeronautics and Space Administration, October 1968. |
| Description: | 1 online resource (20 pages) : illustrations. |
| Language: | English |
| Series: | NASA technical note ; TN D-4796 NASA technical note ; D-4796. |
| Subject: | |
| Format: | E-Resource U.S. Federal Government Document Book |
| URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/12674925 |
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| 100 | 1 | |a Landrum, Emma Jean, |e author. |0 http://id.loc.gov/authorities/names/n82083100 |1 http://viaf.org/viaf/72739040 | |
| 245 | 1 | 0 | |a Effect of shape changes on the aerodynamic characteristics of a twisted and cambered arrow wing at Mach number 2.03 / |c by Emma Jean Landrum and Barrett L. Shrout. |
| 264 | 1 | |a Washington, D.C. : |b National Aeronautics and Space Administration, |c October 1968. | |
| 300 | |a 1 online resource (20 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 | ||
| 338 | |a online resource |b cr |2 rdacarrier |0 http://id.loc.gov/vocabulary/carriers/cr | ||
| 490 | 1 | |a NASA technical note ; |v TN D-4796 | |
| 500 | |a "October 1968." | ||
| 504 | |a Includes bibliographical references (page 7). | ||
| 588 | |a Description based on online resource, PDF version; title from title page (NASA, viewed on Nov. 17, 2020). | ||
| 650 | 0 | |a Aerodynamics, Supersonic. |0 http://id.loc.gov/authorities/subjects/sh85001297 | |
| 650 | 0 | |a Camber (Aerofoils) |0 http://id.loc.gov/authorities/subjects/sh85019077 | |
| 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, Supersonic. |2 fast |0 (OCoLC)fst00798221 | |
| 650 | 7 | |a Camber (Aerofoils) |2 fast |0 (OCoLC)fst00844649 | |
| 650 | 7 | |a Mach number. |2 fast |0 (OCoLC)fst01004756 | |
| 650 | 7 | |a Reynolds number. |2 fast |0 (OCoLC)fst01096833 | |
| 700 | 1 | |a Shrout, Barrett L., |e author. |0 http://id.loc.gov/authorities/names/n82078358 |1 http://viaf.org/viaf/25949367 | |
| 710 | 1 | |a United States. |b National Aeronautics and Space Administration, |e issuing body. |0 http://id.loc.gov/authorities/names/n78087581 |1 http://viaf.org/viaf/146202023 | |
| 710 | 2 | |a Langley Research Center. |0 http://id.loc.gov/authorities/names/n79134855 |1 http://viaf.org/viaf/127305149 | |
| 776 | 0 | 8 | |i Print version: |a Landrum, Emma Jean |t Effect of shape changes on the aerodynamic characteristics of a twisted and cambered arrow wing at Mach number 2.03 |w (OCoLC)52964127 |
| 830 | 0 | |a NASA technical note ; |v D-4796. | |
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