LEADER 02032nam  2200529I  450 
001 9910704205103321
005 20160218115134.0
035   $a(CKB)5470000002439628
035   $a(OCoLC)939619632
035   $a(EXLCZ)995470000002439628
100   $a20160218j199706    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aRotating shake test and modal analysis of a model helicopter rotor blade /$fW. Keats Wilkie, Paul H. Mirick, and Chester W. Langston
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dJune 1997.
215   $a1 online resource (15 pages.) $cillustrations
225 1 $aNASA technical memorandum ;$v4760
300   $aTitle from title screen (viewed on Feb. 18, 2016).
300   $a"June 1997."
300   $a"Performing organizations: NASA Langley Research Center, Hampton, VA [and] Vehicle Technology Center, U.S. Army Research Laboratory, NASA Langley Research Center, Hampton, VA"--Report documentation page.
300   $a"ARL technical report 1389."
320   $aIncludes bibliographical references (page 15).
606   $aRotary wings$2nasat
606   $aHelicopters$2nasat
606   $aAeroelasticity$2nasat
606   $aHovering$2nasat
606   $aTorsion$2nasat
615  7$aRotary wings.
615  7$aHelicopters.
615  7$aAeroelasticity.
615  7$aHovering.
615  7$aTorsion.
700   $aWilkie$b W. Keats$01410623
702   $aMirick$b Paul H.
702   $aLangston$b Chester W.
712 02$aVehicle Technology Center (U.S. Army Research Laboratory)
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910704205103321
996   $aRotating shake test and modal analysis of a model helicopter rotor blade$93531486
997   $aUNINA