01963oam 2200541I 450 991070438220332120170816115022.0(CKB)5470000002439860(OCoLC)755236736(EXLCZ)99547000000243986020110930j199711 ua 0engurbn||||a|a||txtrdacontentcrdamediacrrdacarrierA feasibility study to control airfoil shape using THUNDER /Jennifer L. Pinkerton and Robert W. MosesHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,November 1997.1 online resource (26 pages) illustrationsNASA technical memorandum ;4767Title from title screen (viewed March 2, 2016)."November 1997.""Performing organization: NASA Langley Research Center, Hampton, VA"--Report documentation page.Includes bibliographical references (pages 8-9).Feasibility study to control airfoil shape using thin-layer composite-unimorph ferroelectric driver and sensorActuatorsnasatHysteresisnasatAirfoil profilesnasatPiezoelectricitynasatFerroelectricitynasatActuators.Hysteresis.Airfoil profiles.Piezoelectricity.Ferroelectricity.Pinkerton Jennifer L.1408709Moses Robert W.Langley Research Center,United States.National Aeronautics and Space Administration,OCLCEOCLCEOCLCQOCLCOGPOBOOK9910704382203321A feasibility study to control airfoil shape using THUNDER3493247UNINA