01834oam 2200529 450 991070654870332120171201101145.0(CKB)5470000002456961(OCoLC)862774214(EXLCZ)99547000000245696120131110j200103 ua 0engurbn||||a|a||txtrdacontentcrdamediacrrdacarrierAerodynamic measurements on a large splitter plate for the NASA Langley Transonic Dynamics Tunnel /David M. SchusterHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,March 2001.1 online resource (37 pages) illustrationsNASA/TM ;2001-210828"March 2001.""Performing organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (page 37).Transonic wind tunnelsnasatAerodynamic characteristicsnasatDynamic pressurenasatStatic pressurenasatViscous flownasatWind tunnel testsnasatTransonic wind tunnels.Aerodynamic characteristics.Dynamic pressure.Static pressure.Viscous flow.Wind tunnel tests.Schuster D. M(David M.),1413984Langley Research Center,OCLCEOCLCEOCLCOOCLCFOCLCQGPOBOOK9910706548703321Aerodynamic measurements on a large splitter plate for the NASA Langley Transonic Dynamics Tunnel3511940UNINA