LEADER 01537nam  2200445   450 
001 9910705794003321
005 20170609075749.0
035   $a(CKB)5470000002452463
035   $a(OCoLC)989724350
035   $a(EXLCZ)995470000002452463
100   $a20170609j201701    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aIncreased jet noise due to a "nominally laminar" state of nozzle exit boundary layer /$fK.B.M.Q. Zaman
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dJanuary 2017.
215   $a1 online resource (20 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2017-219440
300   $a"January 2017."
320   $aIncludes bibliographical references (pages 8-9).
606   $aJet aircraft noise$2nasat
606   $aJet nozzles$2nasat
606   $aSound pressure$2nasat
606   $aSubsonic flow$2nasat
606   $aTurbulent boundary layer$2nasat
615  7$aJet aircraft noise.
615  7$aJet nozzles.
615  7$aSound pressure.
615  7$aSubsonic flow.
615  7$aTurbulent boundary layer.
700   $aZaman$b K. B. M. Q$g(Khairul B. M. Q.),$01392412
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910705794003321
996   $aIncreased jet noise due to a "nominally laminar" state of nozzle exit boundary layer$93462706
997   $aUNINA