Application of laminar flow control to supersonic transport configurations.
Saved in:
Imprint: | Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990] |
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Description: | 1 volume. |
Language: | English |
Series: | NASA contractor report ; 181917 NASA contractor report ; NASA CR-181917. |
Subject: | Aerodynamic drag. Boundary layer control. Boundary layer stability. Laminar boundary layer. Pressure distribution. Supersonic transports. Wing planforms. Wings. |
Format: | E-Resource Microform U.S. Federal Government Document Book |
URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/12670274 |
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245 | 0 | 0 | |a Application of laminar flow control to supersonic transport configurations. |
264 | 1 | |a Hampton, Va. : |b National Aeronautics and Space Administration, Langley Research Center, |c [1990] | |
300 | |a 1 volume. | ||
336 | |a text |b txt |2 rdacontent |0 http://id.loc.gov/vocabulary/contentTypes/txt | ||
337 | |a microform |b h |2 rdamedia |0 http://id.loc.gov/vocabulary/mediaTypes/h | ||
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490 | 1 | |a NASA contractor report ; |v 181917 | |
500 | |a "Contract NAS1-15325." | ||
500 | |a "July 1990." | ||
538 | |a Available via Internet from the NTRS web site. Address as of 6/14/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900016628%5F1990016628.pdf; current access is available via PURL. | ||
504 | |a Includes bibliographical references. | ||
650 | 7 | |a Aerodynamic drag. |2 nasat | |
650 | 7 | |a Boundary layer control. |2 nasat | |
650 | 7 | |a Boundary layer stability. |2 nasat | |
650 | 7 | |a Laminar boundary layer. |2 nasat | |
650 | 7 | |a Pressure distribution. |2 nasat | |
650 | 7 | |a Supersonic transports. |2 nasat | |
650 | 7 | |a Wing planforms. |2 nasat | |
650 | 7 | |a Wings. |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 contractor report ; |v NASA CR-181917. | |
856 | 4 | 0 | |u https://purl.fdlp.gov/GPO/LPS60895 |y Government Publishing Office |
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