Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads /
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Author / Creator: | Batina, John T. |
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Imprint: | Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985. |
Description: | 1 volume. |
Language: | English |
Series: | NASA technical memorandum ; 86320 NASA technical memorandum ; 86320. |
Subject: | |
Format: | E-Resource Microform U.S. Federal Government Document Book |
URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/7243330 |
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100 | 1 | |a Batina, John T. |0 http://id.loc.gov/authorities/names/no98120022 |1 http://viaf.org/viaf/61170253 | |
245 | 1 | 0 | |a Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads / |c John T. Batina. |
264 | 1 | |a Washington, D.C. : |b National Aeronautics and Space Administration, Scientific and Technical Information Branch, |c 1985. | |
300 | |a 1 volume. | ||
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490 | 1 | |a NASA technical memorandum ; |v 86320 | |
538 | |a Available via Internet from the NTRS web site. Address as of 07/08/08: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19850010648%5F1985010648.pdf ; current access is available via PURL. | ||
650 | 0 | |a Aerofoils. | |
650 | 0 | |a Camber (Aerofoils) | |
650 | 0 | |a Unsteady flow (Aerodynamics) | |
650 | 0 | |a Aerodynamics, Transonic. | |
650 | 0 | |a Aerodynamic load. | |
650 | 7 | |a Aerodynamic configurations. |2 nasat | |
650 | 7 | |a Airfoils. |2 nasat | |
650 | 7 | |a Computational fluid dynamics. |2 nasat | |
650 | 7 | |a Transonic flow. |2 nasat | |
710 | 1 | |a United States. |b National Aeronautics and Space Administration. |b Scientific and Technical Information Branch. |0 http://id.loc.gov/authorities/names/n78091122 |1 http://viaf.org/viaf/269005387 | |
830 | 0 | |a NASA technical memorandum ; |v 86320. | |
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