01983nam 2200565Ia 450 991070081270332120110927073522.0(CKB)5470000002412894(OCoLC)754787480(EXLCZ)99547000000241289420110927d2011 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierReduced uncertainties in the flutter analysis of the aerostructures test wing[electronic resource] /Chan-gi Pak and Shun-fat LungEdwards, CA :National Aeronautics and Space Administration, Dryden Flight Research Center,[2011]1 online resource (25 pages) illustrations, (some color)NASA/TM ;2011-216421Title from title screen (viewed on Sept. 27, 2011)."January 2011."Includes bibliographical references (pages 13-14).Flutter analysisnasatDynamic structural analysisnasatDesign analysisnasatWingsnasatFinite element methodnasatMultidisciplinary design optimizationnasatFlight testsnasatDynamic modelsnasatTuningnasatFlutter analysis.Dynamic structural analysis.Design analysis.Wings.Finite element method.Multidisciplinary design optimization.Flight tests.Dynamic models.Tuning.Pak Chan-gi1956-1395872Lung Shun-fat1395873Hugh L. Dryden Flight Research Center.GPOGPOBOOK9910700812703321Reduced uncertainties in the flutter analysis of the aerostructures test wing3455056UNINA