01270nam a2200301Ia 4500011443256MiAaHDL20141009010000.0m d cr bn ---auaua920617s1974 dcua b f000 0 eng dsdr-uiuc6396190(OCoLC)26034677ABCABCUIUUTL521.A3525 no. 7814Gloss, Blair B.Effect of canard leading-edge sweep and dihedral angle on the longitudinal and lateral aerodynamic characteristics of a close-coupled canard-wing configuration /by Blair B. Gloss.Washington, D.C. :National Aeronautics and Space Administration ;[Springfield, Va. :For sale by the National Technical Information Service],1974.68 p. :ill. ;27 cm.NASA technical note ;NASA TN D-7814Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12-13).Mode of access: Internet.Stability of airplanes, Lateral.Stability of airplanes, Longitudinal.Leading edges (Aerodynamics)AirplanesWings, Canard.Langley Research Center.01144325620101105090130.020141009010000.020141112165512.02026-02-04T18:42:49Z2026-02-04T18:30:03ZSDR-UIUCUNKNOWNloader.pl-003-020BKsdr-uiuc6396190uiugSDRUIUCuiug.30112106915298UIU6396190UIUUIUC20260204googleuiug.301121069152981974pdbibUS fed doc--NTIS: pubdate < 2020