02094nam 2200517 450 991070387260332120150709162910.0(CKB)5470000002435003(OCoLC)913538436(EXLCZ)99547000000243500320150709j198402 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierExperimental investigation of shock-cell noise reduction for dual-stream nozzles in simulated flight comprehensive data report /K. Yamamoto [and four others]Cincinnati, Ohio :General Electric Company, Aircraft Engine Business Group,February, 1984.1 online resource (2 volumes) illustrationsNASA CR ;168336Title from title screen (viewed on July 9, 2015)."February, 1984."Includes bibliographical references (pages 165-167).v. 1. Test nozzles and acoustic data -- v. 2. Laser velocimeter data, static pressures and shadowgraph photos.Experimental investigation of shock-cell noise reduction for dual-stream nozzles in simulated flight Acoustic measurementnasatNozzle designnasatScale modelsnasatLaser doppler velocimetersnasatShadowgraph photographynasatStatic pressurenasatAcoustic measurement.Nozzle design.Scale models.Laser doppler velocimeters.Shadowgraph photography.Static pressure.Yamamoto K.1412222General Electric Company.Aircraft Engine Business Group,United States.National Aeronautics and Space Administration,GPOGPOBOOK9910703872603321Experimental investigation of shock-cell noise reduction for dual-stream nozzles in simulated flight3505154UNINA