02277nam 2200613 450 991070724020332120160621140035.0(CKB)5470000002463107(OCoLC)951983362(EXLCZ)99547000000246310720160621j199608 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierThe influence of lamination angles on the interior noise levels of an aircraft /Christian M. Fernholz, Jay H. RobinsonHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,August 1996.1 online resource (vi, 83 pages)illustrationsNASA technical memorandum ;110250Title from title screen (viewed June 21, 2016)."August 1996.""Performing organization: NASA Langley Research Center, Hampton, VA"--Report documentation page.Includes bibliographical references (pages 36-39).Aircraft productionnasatCylindrical shellsnasatEquations of motionnasatFinite element methodnasatFrequency rangesnasatThin walled shellsnasatStructural design criterianasatNoise reductionnasatNoise intensitynasatLaminatesnasatAircraft production.Cylindrical shells.Equations of motion.Finite element method.Frequency ranges.Thin walled shells.Structural design criteria.Noise reduction.Noise intensity.Laminates.Fernholz Christian M(Christian Michael),1402976Robinson J. H(Jay Howard),1960-Langley Research Center,United States.National Aeronautics and Space Administration,GPOGPOBOOK9910707240203321The influence of lamination angles on the interior noise levels of an aircraft3474593UNINA