01454nam a2200337Ia 4500011446652MiAaHDL20141009010000.0m d cr bn ---auaua101116s1964 dcua bt f000 0 eng dsdr-uiuc6409726(OCoLC)681621902UIUUIUUIUUNAS 1.15:X-1011Morris, Odell A.Aerodynamic characteristics of a three-engine supersonic transport model having a low-aspect-ratio variable-sweep warped wing /by Odell A. Morris and Dennis E. Fuller.Washington, D.C. :National Aeronautics and Space Administration,1964.59 p. :ill. ;26 cm.NASA technical memorandum ;X-1011"September 1964."Includes bibliographical references (p. 9).Full text also available online. Address as of 11/16/2010:http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19670022815_1967022815.pdf.Mode of access: Internet.Aspect ratio (Aerofoils)Supersonic transport planes.Stability of airplanes, Lateral.Stability of airplanes, Longitudinal.AirplanesWings, Swept-back.Fuller, Dennis E.Langley Research Center.01144665220101116142314.020141009010000.020141112165512.02025-01-01T18:56:39Z2025-01-01T18:30:02ZSDR-UIUCUNKNOWNloader.pl-003-020BKsdr-uiuc6409726uiugSDRUIUCuiug.30112104458051UIU6409726UIUUIUC20250101googleuiug.301121044580511964pdbibUS fed doc