01780nam 2200493I 450 991070257490332120141126100823.0(CKB)5470000002428427(OCoLC)896938005(EXLCZ)99547000000242842720141126j201401 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierActive vibration control for helicopter interior noise reduction using power minimization /J. Mendoza [and four others]Hampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,January 2014.1 online resource (197 pages) color illustrationsNASA-CR ;2014-218147Title from title screen (viewed Nov. 26, 2014)."January 2014."Includes bibliographical references (pages 187-191).Noise reductionnasatRotary wing aircraftnasatAircraft compartmentsnasatOptimal controlnasatStructural vibrationnasatVibration dampingnasatNoise reduction.Rotary wing aircraft.Aircraft compartments.Optimal control.Structural vibration.Vibration damping.Mendoza J.171843Langley Research Center,United States.National Aeronautics and Space Administration,GPOGPOBOOK9910702574903321Active vibration control for helicopter interior noise reduction using power minimization3522951UNINA