01891oam 2200601 450 991070617990332120170823100541.0(CKB)5470000002454625(OCoLC)858260762(EXLCZ)99547000000245462520130912j199905 ua 0engurbn||||a|a||txtrdacontentcrdamediacrrdacarrierA parametric study of accelerations of an airplane due to a wake vortex system /Eric C. StewartHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,May 1999.1 online resource (36 pages) illustrationsNASA/TM ;1999-208745"May 1999.""Performing organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (page 15).AerodynamicsnasatFlow distributionnasatRectangular wingsnasatRollnasatRotationnasatVorticesnasatYawnasatAircraft wakesnasatMathematical modelsnasatAerodynamics.Flow distribution.Rectangular wings.Roll.Rotation.Vortices.Yaw.Aircraft wakes.Mathematical models.Stewart Eric C.1395238Langley Research Center,OCLCEOCLCEOCLCOOCLCFOCLCQGPOBOOK9910706179903321A parametric study of accelerations of an airplane due to a wake vortex system3453417UNINA