Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 /
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Author / Creator: | Pittman, Jimmy L., author. |
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Imprint: | [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980. |
Description: | 1 online resource (113 pages) : illustrations. |
Language: | English |
Series: | NASA technical paper ; 1767 NASA technical paper ; 1767. |
Subject: | |
Format: | E-Resource U.S. Federal Government Document Book |
URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/10914244 |
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086 | 0 | |a NAS 1.60:1767 | |
100 | 1 | |a Pittman, Jimmy L., |e author. |1 http://viaf.org/viaf/72709329 | |
245 | 1 | 0 | |a Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 / |c Jimmy L. Pittman and Gregory D. Riebe. |
264 | 1 | |a [Washington, D.C.] : |b National Aeronautics and Space Administration, Scientific and Technical Information Branch, |c December 1980. | |
300 | |a 1 online resource (113 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 1767 | |
500 | |a Title from title screen (viewed on Aug. 19, 2016). | ||
500 | |a "December 1980." | ||
500 | |a "Performing Organization: NASA Langley Research Center"--Report documentation page. | ||
504 | |a Includes bibliographical references (pages 14-15). | ||
513 | |a Technical paper. | ||
536 | |a National Aeronautics and Space Administration |d 505-31-73-01 |d L-13868 | ||
650 | 7 | |a Aerodynamic characteristics. |2 nasat | |
650 | 7 | |a Aerodynamic configurations. |2 nasat | |
650 | 7 | |a Angle of attack. |2 nasat | |
650 | 7 | |a Hypersonic aircraft. |2 nasat | |
650 | 7 | |a Supersonic aircraft. |2 nasat | |
650 | 7 | |a Aerodynamics, Supersonic. |2 fast |0 http://id.worldcat.org/fast/fst00798221 | |
650 | 7 | |a Hypersonic planes. |2 fast |0 http://id.worldcat.org/fast/fst00965814 | |
650 | 7 | |a Mach number. |2 fast |0 http://id.worldcat.org/fast/fst01004756 | |
650 | 7 | |a Supersonic wind tunnels. |2 fast |0 http://id.worldcat.org/fast/fst01139019 | |
700 | 1 | |a Riebe, Gregory D., |e author. |1 http://viaf.org/viaf/72709338 | |
710 | 2 | |a Langley Research Center. |0 http://id.loc.gov/authorities/names/n79134855 |1 http://viaf.org/viaf/127305149 | |
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 Pittman, Jimmy L. |t Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 |w (OCoLC)7325143 |
776 | 0 | 8 | |i Microfiche version: |a Pittman, Jimmy L. |t Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 |w (OCoLC)711544698 |
830 | 0 | |a NASA technical paper ; |v 1767. | |
856 | 4 | 0 | |u http://purl.fdlp.gov/GPO/gpo71373 |y GPO Documents Without Shelves |
903 | |a HeVa | ||
929 | |a eresource | ||
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928 | |t Library of Congress classification |l Online |c UC-FullText |u http://purl.fdlp.gov/GPO/gpo71373 |z GPO Documents Without Shelves |g ebooks |i 9378751 |