LEADER 01991oam  2200541I  450 
001 9910707306403321
005 20160803155607.0
035   $a(CKB)5470000002464459
035   $a(OCoLC)844685565
035   $a(EXLCZ)995470000002464459
100   $a20130526j199801    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aWind-tunnel evaluation of the effect of blade nonstructural mass distribution on helicopter fixed-system loads /$fMatthew L. Wilbur [and four others]
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dJanuary 1998.
215   $a1 online resource (247 pages) $cillustrations
225 1 $aNASA/TM ;$v1998-206281
225 1 $aARL-TR ;$v1401
300   $aTitle from title screen (viewed Aug. 3, 2016).
300   $a"January 1998."
300   $a"Performing organization: Vehicle Technology Center, U.S. Army Research Laboratory, NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (page 5).
606   $aHelicopters$2nasat
606   $aLoads (forces)$2nasat
606   $aRotary wing aircraft$2nasat
606   $aRotor dynamics$2nasat
606   $aWind tunnel tests$2nasat
615  7$aHelicopters.
615  7$aLoads (forces)
615  7$aRotary wing aircraft.
615  7$aRotor dynamics.
615  7$aWind tunnel tests.
700   $aWilbur$b Matthew L.$01389368
712 02$aLangley Research Center,
712 02$aVehicle Technology Center (U.S. Army Research Laboratory),
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCO
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910707306403321
996   $aWind-tunnel evaluation of the effect of blade nonstructural mass distribution on helicopter fixed-system loads$93440835
997   $aUNINA