LEADER 01957nam  2200493I  450 
001 9910702488403321
005 20130212085932.0
035   $a(CKB)5470000002427281
035   $a(OCoLC)827271607
035   $a(EXLCZ)995470000002427281
100   $a20130212d2012      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aNearfield unsteady pressures at cruise Mach numbers for a model scale counter-rotation open rotor /$fDavid B. Stephen
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d2012.
215   $a1 online resource (11 pages) $cillustrations (some color)
225 1 $aNASA/TM ;$v2012-217672
300   $aTitle from title screen (viewed on Jan. 14, 2013).
300   $a"September 2012."
300   $a"Prepared for the 18th Aeroacoustics Conference cosponsored by the American Institute of Aeronautics and Astronautics and Confederation of European Aerospace Societies, Colorado Springs, Colorado, June 4-6, 2012."
300   $a"AIAA-2012-2264."
320   $aIncludes bibliographical references (page 11).
606   $aCounter rotation$2nasat
606   $aFlow measurement$2nasat
606   $aNoise generators$2nasat
606   $aRotors$2nasat
606   $aAngular distribution$2nasat
615  7$aCounter rotation.
615  7$aFlow measurement.
615  7$aNoise generators.
615  7$aRotors.
615  7$aAngular distribution.
700   $aStephens$b David B.$01404359
712 02$aNASA Glenn Research Center,
712 12$aAIAA/CEAS Aeroacoustics Conference$d(18th :$f2012 :$eColorado Springs, Colo.)
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702488403321
996   $aNearfield unsteady pressures at cruise Mach numbers for a model scale counter-rotation open rotor$93526871
997   $aUNINA