LEADER 01913nam  2200553Ia 450 
001 9910697014003321
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035   $a(CKB)5470000002384766
035   $a(OCoLC)649840609
035   $a(EXLCZ)995470000002384766
100   $a20100723d2005      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aLoads and performance data from a wind-tunnel test of generic model helicopter rotor blades$b[electronic resource] /$fWilliam T. Yeager, Jr., and Matthew L. Wilbur
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[2005]
215   $a1 online resource (548 pages) $cillustrations
225 1 $aNASA/TP ;$v2005-213937
300   $aTitle from title screen (viewed on July 22, 2010).
300   $a"November 2005."
320   $aIncludes bibliographical references (pages 6-7).
410  0$aNASA technical paper ;$v213937.
606   $aRotary wings$2nasat
606   $aHelicopters$2nasat
606   $aVibratory loads$2nasat
606   $aRotors$2nasat
606   $aShafts (machine elements)$2nasat
606   $aTorsion$2nasat
606   $aRadial distribution$2nasat
606   $aAngle of attack$2nasat
615  7$aRotary wings.
615  7$aHelicopters.
615  7$aVibratory loads.
615  7$aRotors.
615  7$aShafts (machine elements)
615  7$aTorsion.
615  7$aRadial distribution.
615  7$aAngle of attack.
700   $aYeager$b William T$01398153
701   $aWilbur$b Matthew L$01389368
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910697014003321
996   $aLoads and performance data from a wind-tunnel test of generic model helicopter rotor blades$93469582
997   $aUNINA