01619nam a2200361Ia 4500011446698MiAaHDL20141009010000.0m d cr bn ---auaua101116s1961 dcua bt f000 0 eng sdr-uiuc6409356(OCoLC)681548627UIUUIUUIUUNAS 1.15:X-521Morris, Odell A.Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a V/STOL airplane configuration with a variable-sweep wing and with a skewed wing design /by Odell A. Morris and Gerald V. Foster.Washington, D.C. :National Aeronautics and Space Administration,1961.28 p. :ill. ;26 cm.NASA technical memorandum ;X-521"April 1961."Cover title.Includes bibliographical references (p. 7).Full text also available online. Address as of 11/16/2010:http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19660013086_1966013086.pdf.Mode of access: Internet.Supersonic wind tunnelsTesting.Angle of attack (Aerodynamics)Stability of airplanes, LateralTesting.Stability of airplanes, LongitudinalTesting.AirplanesWings, Swept-backTesting.Hypersonic planes, MilitaryTesting.Foster, Gerald V.Langley Research Center.01144669820101116094917.020141009010000.020141112165512.02025-01-01T18:56:47Z2025-01-01T18:30:02ZSDR-UIUCUNKNOWNloader.pl-003-020BKsdr-uiuc6409356uiugSDRUIUCuiug.30112104504748UIU6409356UIUUIUC20250101googleuiug.301121045047481961pdbibUS fed doc