01925nam 2200481 450 991070438250332120160302105706.0(CKB)5470000002439857(OCoLC)942651780(EXLCZ)99547000000243985720160302j199612 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierSurface-pressure and flow-visualization data at Mach number of 1.60 for three 65° delta wings varying in leading-edge radius and camber /S. Naomi McMillin [and five others]Hampton, VA :National Aeronautics and Space Administration, Langley Research Center,December 1996.1 online resource (iii, 262 pages) illustrationsNASA technical memorandum ;4673Title from title screen (viewed March 2, 2016)."December 1996.""Performing organization: NASA Langley Research Center, Hampton, VA"--Report documentation page.Includes bibliographical references (page 262).Delta wingsnasatFlow visualizationnasatLeading edgesnasatReynolds numbernasatBoundary layer transitionnasatDelta wings.Flow visualization.Leading edges.Reynolds number.Boundary layer transition.McMillin S. Naomi(Susan Naomi),1419322Langley Research Center,United States.National Aeronautics and Space Administration,GPOGPOBOOK9910704382503321Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65° delta wings varying in leading-edge radius and camber3533368UNINA