01830nam 2200481 450 991070719680332120160426151029.0(CKB)5470000002461525(OCoLC)947889608(EXLCZ)99547000000246152520160426j201512 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierCalculated low-speed steady and time-dependent aerodynamic derivatives for some airfoils using a discrete vortex method /Donald R. RileyHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,December 2015.1 online resource (61 pages) illustrationsNASA/TM ;2015-218998Title from title screen (viewed April 26, 2016)."December 2015.""Performing organization: NASA Langley Research Center, Hampton, VA"--Report documentation page.Includes bibliographical references (page 14).Aerodynamic coefficientsnasatAerodynamic stabilitynasatAirfoilsnasatTime dependencenasatVorticesnasatAerodynamic coefficients.Aerodynamic stability.Airfoils.Time dependence.Vortices.Riley Donald R.1386410Langley Research Center,United States.National Aeronautics and Space Administration,GPOGPOBOOK9910707196803321Calculated low-speed steady and time-dependent aerodynamic derivatives for some airfoils using a discrete vortex method3544733UNINA