01712nam 2200505I 450 991070273430332120150203131956.0(CKB)5470000002430858(OCoLC)902680688(EXLCZ)99547000000243085820150203j201409 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierAeroelastic tailoring via tow steered composites /Bret K. Stanford, Christine V. JutteHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,September 2014.1 online resource (25 pages) color illustrationsNASA/TM ;2014-218517Title from title screen (viewed Feb. 3, 2015)."September 2014."Includes bibliographical references (pages 24-25).AeroelasticitynasatLaminatesnasatStiffness matrixnasatTransverse loadsnasatHigh aspect rationasatAerodynamic loadsnasatAeroelasticity.Laminates.Stiffness matrix.Transverse loads.High aspect ratio.Aerodynamic loads.Stanford Bret K.1405266Jutte Christine V.Langley Research Center,United States.National Aeronautics and Space Administration,GPOGPOBOOK9910702734303321Aeroelastic tailoring via tow steered composites3542440UNINA