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001 9910714047303321
005 20201211103447.0
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035   $a(OCoLC)761236134
035   $a(EXLCZ)995470000002507174
100   $a20111115j196902    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA parametric study of blade-motion stability boundaries for an articulated rotor /$fby Julian L. Jenkins, Jr
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dFebruary 1969.
215   $a1 online resource (28 pages) $cillustrations
225 1 $aNASA technical note ;$vD-5032
300   $a"February 1969."
320   $aIncludes bibliographical references (page 14).
606   $aRotors (Helicopters)$xAerodynamics
606   $aBlades
606   $aSpace vehicles
606   $aBlades$2fast
606   $aRotors (Helicopters)$xAerodynamics$2fast
606   $aSpace vehicles$2fast
615  0$aRotors (Helicopters)$xAerodynamics.
615  0$aBlades.
615  0$aSpace vehicles.
615  7$aBlades.
615  7$aRotors (Helicopters)$xAerodynamics.
615  7$aSpace vehicles.
700   $aJenkins$b Julian L.$01396445
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aLangley Research Center.
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCO
801  2$bOCLCQ
801  2$bOCLCA
801  2$bCOP
801  2$bGPO
906   $aBOOK
912   $a9910714047303321
996   $aA parametric study of blade-motion stability boundaries for an articulated rotor$93456593
997   $aUNINA