01790nam 2200493I 450 991070792820332120170525133947.0(CKB)5470000002469289(OCoLC)972501458(EXLCZ)99547000000246928920170214j201611 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierWind tunnel test of a risk-reduction wing/fuselage model to examine juncture-flow phenomena /Michael A. Kegerise and Dan H. NeuhartHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,November 2016.1 online resource (118 pages) color illustrationsNASA/TM ;2016-219348"November 2016.""Performing organization: NASA Langley Research Center" Report documentation page.Includes bibliographical references (pages 30-31).Body-wing configurationsnasatFlow distributionnasatLaser doppler velocimetersnasatReynolds numbernasatSubsonic wind tunnelsnasatWind tunnel modelsnasatBody-wing configurations.Flow distribution.Laser doppler velocimeters.Reynolds number.Subsonic wind tunnels.Wind tunnel models.Kegerise Michael A.1397448Neuhart Dan H(Dan Howard),1952-Langley Research Center,GPOGPOBOOK9910707928203321Wind tunnel test of a risk-reduction wing3503867UNINA