01913nam 2200553Ia 450 991069701400332120230902161717.0(CKB)5470000002384766(OCoLC)649840609(EXLCZ)99547000000238476620100723d2005 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierLoads and performance data from a wind-tunnel test of generic model helicopter rotor blades[electronic resource] /William T. Yeager, Jr., and Matthew L. WilburHampton, Va. :National Aeronautics and Space Administration, Langley Research Center,[2005]1 online resource (548 pages) illustrationsNASA/TP ;2005-213937Title from title screen (viewed on July 22, 2010)."November 2005."Includes bibliographical references (pages 6-7).NASA technical paper ;213937.Rotary wingsnasatHelicoptersnasatVibratory loadsnasatRotorsnasatShafts (machine elements)nasatTorsionnasatRadial distributionnasatAngle of attacknasatRotary wings.Helicopters.Vibratory loads.Rotors.Shafts (machine elements)Torsion.Radial distribution.Angle of attack.Yeager William T1398153Wilbur Matthew L1389368Langley Research Center.GPOGPOBOOK9910697014003321Loads and performance data from a wind-tunnel test of generic model helicopter rotor blades3469582UNINA