01803oam 2200529 450 991070616900332120170911123159.0(CKB)5470000002454735(OCoLC)858263714(EXLCZ)99547000000245473520130912j199909 ua 0engurbn||||a|a||txtrdacontentcrdamediacrrdacarrierAerodynamic characteristics and control effectiveness of the HL-20 lifting body configuration at Mach 10 in air /William I. ScallionHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,September 1999.1 online resource (54 pages) illustrationsNASA TM- ;1999-209357"September 1999.""Performing organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (page 9).ControllabilitynasatEffectivenessnasatLifting bodiesnasatScale modelsnasatWind tunnel testsnasatElevonsnasatControllability.Effectiveness.Lifting bodies.Scale models.Wind tunnel tests.Elevons.Scallion William I.1395362Langley Research Center,OCLCEOCLCEOCLCOOCLCFOCLCQGPOBOOK9910706169003321Aerodynamic characteristics and control effectiveness of the HL-20 lifting body configuration at Mach 10 in air3453744UNINA