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035   $a(EXLCZ)995470000002461399
100   $a20110224j199611    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFlight and static exhaust flow properties of an F110-GE-129 engine in an F-16XL airplane during acoustic tests /$fJon K. Holzman, Lannie D. Webb, and Frank W. Burcham, Jr
210  1$aEdwards, California.:$cNational Aeronautics and Space Administration, Dryden Flight Research Center,$dNovember 1996.
215   $a1 online resource (iv, 26 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v104326
300   $aTitle from title screen (viewed April 5, 2016).
300   $a"November 1996."
300   $a"Performing organization: NASA Dryden Flight Research Center, Edwards, California"--Report documentation page.
320   $aIncludes bibliographical references (page 26).
606   $aAcoustic measurement$2nasat
606   $aAircraft noise$2nasat
606   $aEngine noise$2nasat
606   $aExhaust gases$2nasat
606   $aJet engines$2nasat
615  7$aAcoustic measurement.
615  7$aAircraft noise.
615  7$aEngine noise.
615  7$aExhaust gases.
615  7$aJet engines.
700   $aHolzman$b Jon K.$01404714
702   $aWebb$b Lannie D.
702   $aBurcham$b Frank W.
712 02$aNASA Dryden Flight Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bSSN
801  1$bSSN
801  2$bGPO
906   $aBOOK
912   $a9910707009303321
996   $aFlight and static exhaust flow properties of an F110-GE-129 engine in an F-16XL airplane during acoustic tests$93479818
997   $aUNINA