01893nam 2200529 a 450 991070081820332120111024122806.0(CKB)5470000002412838(OCoLC)758377228(EXLCZ)99547000000241283820111024d2011 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierMeasured sonic boom signatures above and below the XB-70 airplane flying at Mach 1.5 and 37,000 feet[electronic resource] /Domenic J. Maglieri and Herbert R. Henderson, Ana F. TinettiHampton, Va. :National Aeronautics and Space Administration, Langley Research Center,[2011]1 online resource (65 pages) illustrationsNASA/CR ;2011-217077Title from title screen (viewed on Oct. 24, 2011)."April 2011."Includes bibliographical references (pages 26-28).F-104 aircraftnasatFlow distributionnasatSonic boomsnasatSupersonic speednasatB-70 aircraftnasatShock wavesnasatWind tunnel testsnasatF-104 aircraft.Flow distribution.Sonic booms.Supersonic speed.B-70 aircraft.Shock waves.Wind tunnel tests.Maglieri Domenic J1398407Henderson Herbert R1414725Tinetti Ana Fiorella1962-1389734Langley Research Center.GPOGPOBOOK9910700818203321Measured sonic boom signatures above and below the XB-70 airplane flying at Mach 1.5 and 37,000 feet3514798UNINA