LEADER 01615nam  2200469I  450 
001 9910705713903321
005 20170707085648.0
035   $a(CKB)5470000002453272
035   $a(OCoLC)992989283
035   $a(EXLCZ)995470000002453272
100   $a20170707j201705    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aInlet acoustic data from a high bypass ratio turbofan rotor in an internal flow component test facility /$fRichard F. Bozak
210  1$aCleveland, Ohio:$cNational Aeronautics and Space Administration, Glenn Research Center,$dMay 2017.
215   $a1 online resource (6 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2017-219489
300   $a"May 2017."
320   $aIncludes bibliographical references (page 2).
606   $aAcoustic properties$2nasat
606   $aAerodynamic characteristics$2nasat
606   $aBypass ratio$2nasat
606   $aNoise reduction$2nasat
606   $aRotors$2nasat
606   $aTurbofan engines$2nasat
615  7$aAcoustic properties.
615  7$aAerodynamic characteristics.
615  7$aBypass ratio.
615  7$aNoise reduction.
615  7$aRotors.
615  7$aTurbofan engines.
700   $aBozak$b Richard F.$01405259
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910705713903321
996   $aInlet acoustic data from a high bypass ratio turbofan rotor in an internal flow component test facility$93494649
997   $aUNINA