Supersonic aerodynamic characteristics of some reentry concepts for angles of attack to 90⁰ /
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Author / Creator: | Spearman, M. Leroy. |
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Imprint: | Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985] |
Description: | 1 volume. |
Language: | English |
Series: | NASA technical memorandum ; 87645 NASA technical memorandum ; 87645. |
Subject: | |
Format: | E-Resource Microform U.S. Federal Government Document Book |
URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/6808503 |
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100 | 1 | |a Spearman, M. Leroy. |0 http://id.loc.gov/authorities/names/n84213710 |1 http://viaf.org/viaf/94547032 | |
245 | 1 | 0 | |a Supersonic aerodynamic characteristics of some reentry concepts for angles of attack to 90⁰ / |c M. Leroy Spearman. |
264 | 1 | |a Hampton, Va. : |b National Aeronautics and Space Administration, Langley Research Center, |c [1985] | |
300 | |a 1 volume. | ||
336 | |a text |b txt |2 rdacontent |0 http://id.loc.gov/vocabulary/contentTypes/txt | ||
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490 | 1 | |a NASA technical memorandum ; |v 87645 | |
538 | |a Available via Internet from the NTRS web site. Address as of 8/39/07: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19860006773%5F1986006773.pdf ; current access is available via PURL. | ||
650 | 0 | |a Space vehicles. | |
650 | 0 | |a Aerodynamics, Supersonic. | |
650 | 7 | |a Angle of attack. |2 nasat | |
650 | 7 | |a Cambered wings. |2 nasat | |
650 | 7 | |a Circular cones. |2 nasat | |
650 | 7 | |a Delta wings. |2 nasat | |
650 | 7 | |a Mach number. |2 nasat | |
650 | 7 | |a Planforms. |2 nasat | |
650 | 7 | |a Reentry vehicles. |2 nasat | |
650 | 7 | |a Supersonic airfoils. |2 nasat | |
650 | 7 | |a Transatmospheric vehicles. |2 nasat | |
710 | 2 | |a Langley Research Center. |0 http://id.loc.gov/authorities/names/n79134855 |1 http://viaf.org/viaf/127305149 | |
830 | 0 | |a NASA technical memorandum ; |v 87645. | |
856 | 4 | 0 | |u https://purl.fdlp.gov/GPO/LPS85587 |y Government Publishing Office |
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