01266cam a2200301Ii 4500011425084MiAaHDL20141013010000.0m d cr bn ---auaua790327s1978 dcua b f000 0 eng dsdr-uiuc6360963(OCoLC)478675922161GPOGPOOCLABCOCLCQUIUUTL521.3.T4A3 no. 78686830-D (microfiche)NAS 1.15:78686Gloss, Blair B.Effect of camber on the trimmed lift capability of a close-coupled canard-wing configuration /Blair B. Gloss, Langley Research Center.[Washington] :National Aeronautics and Space Administration :Scientific and Technical Information Office ;Springfield, Va. :For sale by the National Technical Information Service,1978.91 p. :ill. ;27 cm.NASA technical memorandum ;78686July 1978.Includes bibliographical references.Mode of access: Internet.AirplanesWings, Canard.Camber (Aerofoils)Langley Research Center.United States.National Aeronautics and Space Administration.Scientific and Technical Information Office.01142508420101005083037.020141013010000.020141112173021.02025-01-01T19:24:19Z2025-01-01T18:30:02ZSDR-UIUCUNKNOWNloader.pl-003-020BKsdr-uiuc6360963uiugSDRUIUCuiug.30112106660506UIU6360963UIUUIUC20250101googleuiug.301121066605061978pdbibUS fed doc--NTIS: pubdate < 2020