LEADER 02086nam  2200541I  450 
001 9910702431703321
005 20140709095534.0
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035   $a(OCoLC)883208686
035   $a(EXLCZ)995470000002427854
100   $a20140709j201308    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aUpdated assessment of an open rotor airplane using an advanced blade design /$fEric S. Hendricks [and four others]
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dAugust 2013.
215   $a1 online resource (13 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2013-218074
300   $aTitle from title screen (viewed July 9, 2014).
300   $a"August 2013."
300   $a"Prepared for the 49th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE San Jose, California, July 14-17, 2013."
300   $a"AIAA-2013-3628."
320   $aIncludes bibliographical references (pages 12-13).
606   $aContrarotating propellers$2nasat
606   $aFuel consumption$2nasat
606   $aLow noise$2nasat
606   $aNoise intensity$2nasat
606   $aNoise prediction (aircraft)$2nasat
606   $aPropulsion system configurations$2nasat
606   $aPropulsion system performance$2nasat
615  7$aContrarotating propellers.
615  7$aFuel consumption.
615  7$aLow noise.
615  7$aNoise intensity.
615  7$aNoise prediction (aircraft)
615  7$aPropulsion system configurations.
615  7$aPropulsion system performance.
700   $aHendricks$b Eric S.$01402593
712 02$aNASA Glenn Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702431703321
996   $aUpdated assessment of an open rotor airplane using an advanced blade design$93473451
997   $aUNINA