LEADER 02045nam  2200553Ia 450 
001 9910696929403321
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035   $a(CKB)5470000002383600
035   $a(OCoLC)642331797
035   $a(EXLCZ)995470000002383600
100   $a20100618d2009      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aBroadband shock noise in internally-mixed dual-stream jets$b[electronic resource] /$fJames E. Bridges ; prepared for the 15th Aeroacoustics Conference (30th AIAA Aeroacoustics Conference) cosponsored by AIAA and CEAS, Miami, Florida, May 11-13, 2009
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2009]
215   $a1 online resource (17 pages) $cillustrations
225 1 $aNASA TM- ;$v2009-215817
300   $aTitle from title screen (viewed on June 17, 2010).
300   $a"November 2009."
300   $a"AIAA-2009-3210."
320   $aIncludes bibliographical references (page 17).
410  0$aNASA technical memorandum ;$v2009-215817.
606   $aAerodynamic noise$2nasat
606   $aNozzle flow$2nasat
606   $aNoise measurement$2nasat
606   $aFlow noise$2nasat
606   $aShock waves$2nasat
606   $aBypass ratio$2nasat
606   $aShear layers$2nasat
615  7$aAerodynamic noise.
615  7$aNozzle flow.
615  7$aNoise measurement.
615  7$aFlow noise.
615  7$aShock waves.
615  7$aBypass ratio.
615  7$aShear layers.
700   $aBridges$b James E$01394301
712 02$aNASA Glenn Research Center.
712 12$aAIAA/CEAS Aeroacoustics Conference$d(15th :$f2009 :$eMiami, Fla.)
712 12$aAIAA Aeroacoustics Conference$d(30th :$f2009 :$eMiami, Fla.)
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910696929403321
996   $aBroadband shock noise in internally-mixed dual-stream jets$93451473
997   $aUNINA