02022nam 2200577 450 991070614370332120170906140120.0(CKB)5470000002454991(OCoLC)1003045325(EXLCZ)99547000000245499120170906j199912 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierNacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds /Robert J. MackHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,December 1999.1 online resource (15 pages) illustrationsNASA/TM ;1999-209534"December 1999.""Performing organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (pages 13-15).Aerodynamic characteristicsnasatBody-wing configurationsnasatNacellesnasatSonic boomsnasatWingsnasatAerodynamic configurationsnasatSupersonic flightnasatAerodynamic noisenasatNoise reductionnasatWind tunnel testsnasatAerodynamic characteristics.Body-wing configurations.Nacelles.Sonic booms.Wings.Aerodynamic configurations.Supersonic flight.Aerodynamic noise.Noise reduction.Wind tunnel tests.Mack Robert J.1408827Langley Research Center,GPOGPOBOOK9910706143703321Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds3512804UNINA