LEADER 02155oam  2200529   450 
001 9910704204403321
005 20160219102337.0
035   $a(CKB)5470000002439635
035   $a(OCoLC)74226211
035   $a(EXLCZ)995470000002439635
100   $a20080513j199705    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aPerformance and vibratory loads data from a wind-tunnel test of a model helicopter main-rotor blade with a paddle-type tip /$fWilliam T. Yeager, Jr. [and four others]
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dMay 1997.
215   $a1 online resource (23 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v4754
225 1 $aARL technical report ;$v1283
300   $aTitle from title screen (viewed on Feb. 19, 2016).
300   $a"May 1997."
300   $a"Performing organizations: Vehicle Technology Center, U.S. Army Research Laboratory, NASA Langley Research Center; Joint Research Program Office, Aeroflightdynamics Directorate, U.S. Army Aviation and Troop Command, NASA Langley Research Center"--Report documentation page.
300   $a"ATCOM technical report 97-A-006."
320   $aIncludes bibliographical references (page 6).
606   $aRotary wings$2nasat
606   $aVibratory loads$2nasat
606   $aTransonic wind tunnels$2nasat
606   $aPaddles$2nasat
606   $aRotors$2nasat
615  7$aRotary wings.
615  7$aVibratory loads.
615  7$aTransonic wind tunnels.
615  7$aPaddles.
615  7$aRotors.
700   $aYeager$b William T.$01398153
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bDTICE
801  1$bDTICE
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910704204403321
996   $aPerformance and vibratory loads data from a wind-tunnel test of a model helicopter main-rotor blade with a paddle-type tip$93490132
997   $aUNINA