In-flight boundary-layer measurements on a hollow cylinder at a Mach number of 3.0 /
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| Author / Creator: | Quinn, Robert D., author. |
|---|---|
| Imprint: | [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November1980. |
| Description: | 1 online resource (49 pages) : illustrations. |
| Language: | English |
| Series: | NASA technical paper ; 1764 NASA technical paper ; 1764. |
| Subject: | |
| Format: | E-Resource U.S. Federal Government Document Book |
| URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/10914238 |
MARC
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| 100 | 1 | |a Quinn, Robert D., |e author. |0 http://id.loc.gov/authorities/names/n81041539 |1 http://viaf.org/viaf/106551580 | |
| 245 | 1 | 0 | |a In-flight boundary-layer measurements on a hollow cylinder at a Mach number of 3.0 / |c Robert D. Quinn and Leslie Gong. |
| 264 | 1 | |a [Washington, D.C.] : |b National Aeronautics and Space Administration, Scientific and Technical Information Branch, |c November1980. | |
| 300 | |a 1 online resource (49 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 NASA technical paper ; |v 1764 | |
| 500 | |a Title from title screen (viewed on Aug. 18, 2016). | ||
| 500 | |a "November1980." | ||
| 500 | |a "Performing Organization: NASA Dryden Flight Research Center"--Report documentation page. | ||
| 504 | |a Includes bibliographical references (pages 18-19). | ||
| 513 | |a Technical paper. | ||
| 536 | |a National Aeronautics and Space Administration |h 505-43-24 | ||
| 536 | |d H-1101 | ||
| 650 | 7 | |a Heat transfer coefficients. |2 nasat | |
| 650 | 7 | |a Mach number. |2 nasat | |
| 650 | 7 | |a Reynolds number. |2 nasat | |
| 650 | 7 | |a Shear flow. |2 nasat | |
| 650 | 7 | |a Aerodynamic heating. |2 fast |0 http://id.worldcat.org/fast/fst00798175 | |
| 650 | 7 | |a Heat |x Transmission. |2 fast |0 http://id.worldcat.org/fast/fst00953826 | |
| 650 | 7 | |a Turbulent boundary layer. |2 fast |0 http://id.worldcat.org/fast/fst01159225 | |
| 700 | 1 | |a Gong, Leslie, |e author. |0 http://id.loc.gov/authorities/names/n81041546 |1 http://viaf.org/viaf/45619165 | |
| 710 | 2 | |a Hugh L. Dryden Flight Research Center. |0 http://id.loc.gov/authorities/names/n79084677 |1 http://viaf.org/viaf/126658266 | |
| 710 | 1 | |a United States. |b National Aeronautics and Space Administration. |b Scientific and Technical Information Branch, |e issuing body. |0 http://id.loc.gov/authorities/names/n78091122 |1 http://viaf.org/viaf/269005387 | |
| 776 | 0 | 8 | |i Print version: |a Quinn, Robert D. |t In-flight boundary-layer measurements on a hollow cylinder at a Mach number of 3.0 |w (OCoLC)7373501 |
| 776 | 0 | 8 | |i Microfiche version: |a Quinn, Robert D. |t In-flight boundary-layer measurements on a hollow cylinder at a Mach number of 3.0 |w (OCoLC)711544742 |
| 830 | 0 | |a NASA technical paper ; |v 1764. | |
| 856 | 4 | 0 | |u http://purl.fdlp.gov/GPO/gpo71370 |y GPO Documents Without Shelves |
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