A method for determining the total drag of a pointed body of revolution in supersonic flow with turbulent boundary layer /
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| Author / Creator: | Jackson, Charlie M., author. |
|---|---|
| Imprint: | Washington, D.C. : National Aeronautics and Space Administration, March 1969. |
| Description: | 1 online resource (65 pages) : illustrations. |
| Language: | English |
| Series: | NASA technical note ; TN D-5046 NASA technical note ; D-5046. |
| Subject: | Drag (Aerodynamics) Boundary layer. Boundary layer. Drag (Aerodynamics) |
| Format: | E-Resource U.S. Federal Government Document Book |
| URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/12675081 |
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| 100 | 1 | |a Jackson, Charlie M., |e author. |0 http://id.loc.gov/authorities/names/n82208706 |1 http://viaf.org/viaf/6291594 | |
| 245 | 1 | 2 | |a A method for determining the total drag of a pointed body of revolution in supersonic flow with turbulent boundary layer / |c by Charlie M. Jackson, Jr., and Rudeen S. Smith. |
| 264 | 1 | |a Washington, D.C. : |b National Aeronautics and Space Administration, |c March 1969. | |
| 300 | |a 1 online resource (65 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-5046 | |
| 500 | |a "March 1969." | ||
| 504 | |a Includes bibliographical references (pages 48-49). | ||
| 588 | |a Description based on online resource, PDF version; title from title page (NASA, viewed on Nov. 4, 2020). | ||
| 650 | 0 | |a Drag (Aerodynamics) |0 http://id.loc.gov/authorities/subjects/sh85039270 | |
| 650 | 0 | |a Boundary layer. |0 http://id.loc.gov/authorities/subjects/sh85016095 | |
| 650 | 7 | |a Boundary layer. |2 fast |0 (OCoLC)fst00837095 | |
| 650 | 7 | |a Drag (Aerodynamics) |2 fast |0 (OCoLC)fst00897351 | |
| 700 | 1 | |a Smith-Taylor, Rudeen, |e author. |0 http://id.loc.gov/authorities/names/no2008149356 |1 http://viaf.org/viaf/29358974 | |
| 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 Jackson, Charlie M. |t Method for determining the total drag of a pointed body of revolution in supersonic flow with turbulent boundary layer |w (OCoLC)646012187 |
| 830 | 0 | |a NASA technical note ; |v D-5046. | |
| 856 | 4 | 0 | |u https://purl.fdlp.gov/GPO/gpo146988 |y Government Publishing Office |
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