LEADER 02094nam  2200517   450 
001 9910703872603321
005 20150709162910.0
035   $a(CKB)5470000002435003
035   $a(OCoLC)913538436
035   $a(EXLCZ)995470000002435003
100   $a20150709j198402    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aExperimental investigation of shock-cell noise reduction for dual-stream nozzles in simulated flight $ecomprehensive data report /$fK. Yamamoto [and four others]
210  1$aCincinnati, Ohio :$cGeneral Electric Company, Aircraft Engine Business Group,$dFebruary, 1984.
215   $a1 online resource (2 volumes) $cillustrations
225 1 $aNASA CR ;$v168336
300   $aTitle from title screen (viewed on July 9, 2015).
300   $a"February, 1984."
320   $aIncludes bibliographical references (pages 165-167).
327   $av. 1. Test nozzles and acoustic data -- v. 2. Laser velocimeter data, static pressures and shadowgraph photos.
517   $aExperimental investigation of shock-cell noise reduction for dual-stream nozzles in simulated flight 
606   $aAcoustic measurement$2nasat
606   $aNozzle design$2nasat
606   $aScale models$2nasat
606   $aLaser doppler velocimeters$2nasat
606   $aShadowgraph photography$2nasat
606   $aStatic pressure$2nasat
615  7$aAcoustic measurement.
615  7$aNozzle design.
615  7$aScale models.
615  7$aLaser doppler velocimeters.
615  7$aShadowgraph photography.
615  7$aStatic pressure.
700   $aYamamoto$b K.$01412222
712 02$aGeneral Electric Company.$bAircraft Engine Business Group,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910703872603321
996   $aExperimental investigation of shock-cell noise reduction for dual-stream nozzles in simulated flight$93505154
997   $aUNINA