LEADER 02021nam  2200529I  450 
001 9910706550103321
005 20171201085000.0
035   $a(CKB)5470000002456947
035   $a(OCoLC)1013716679
035   $a(EXLCZ)995470000002456947
100   $a20171201j200104    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aDesign and integration of a rotor alone nacelle for acoustic fan testing /$fTony D. Shook [and five others]
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dApril 2001.
215   $a1 online resource (8 pages) $cillustrations
225 1 $aNASA/TM ;$v2001-210820
300   $a"April 2001."
300   $a"Prepared for the 39th Aerospace Sciences Meeting and Exhibit sponsored by the American Institute of Aeronautics and Astronautics, Reno, Nevada, January 8-11, 2001."
300   $a"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.
300   $a"AIAA-2001-1058."
320   $aIncludes bibliographical references (page 8).
606   $aRotor blades (turbomachinery)$2nasat
606   $aRotors$2nasat
606   $aFan blades$2nasat
606   $aTurbomachine blades$2nasat
606   $aNacelles$2nasat
606   $aAerodynamic configurations$2nasat
606   $aDesign analysis$2nasat
615  7$aRotor blades (turbomachinery)
615  7$aRotors.
615  7$aFan blades.
615  7$aTurbomachine blades.
615  7$aNacelles.
615  7$aAerodynamic configurations.
615  7$aDesign analysis.
700   $aShook$b Tony D.$01403639
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910706550103321
996   $aDesign and integration of a rotor alone nacelle for acoustic fan testing$93476727
997   $aUNINA