02127nam 2200541 450 991070652090332120171213082055.0(CKB)5470000002457242(OCoLC)1015309431(EXLCZ)99547000000245724220171213j199912 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierSubsonic investigation of a leading-edge boundary layer contol suction system on a high-speed civil transport configuration /Bryan A. Campbell [and seven others]Hampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,December 1999.1 online resource (128 pages) illustrationsNASA/TM ;1999-209700"December 1999.""Performing organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (page 128).Subsonic investigation of a leading-edge boundary layer control suction system on a high-speed civil transport configurationBoundary layer controlnasatLeading edgesnasatWind tunnel testsnasatFlaps (control surfaces)nasatPressure effectsnasatSubsonic speednasatSupersonic transportsnasatAerodynamic configurationsnasatBoundary layer control.Leading edges.Wind tunnel tests.Flaps (control surfaces)Pressure effects.Subsonic speed.Supersonic transports.Aerodynamic configurations.Campbell Bryan A.1395236Langley Research Center,GPOGPOBOOK9910706520903321Subsonic investigation of a leading-edge boundary layer contol suction system on a high-speed civil transport configuration3539148UNINA