Cruise noise of an advanced counterrotation turboprop measured from an adjacent aircraftAcoustic test results are presented for a full-scale counterrotation demonstrator engine installed on a Boeing 727 aircraft in place of the right-side turbofan engine. Sideline acoustic data were acquired from a Learjet chase aircraft instrumented with noise and wing-tip flush mount microphones. Data are presented for a 47.2-m sideline at several engine operating conditions and flight Mach numbers of 0.50 and 0.72.
Document ID
19890027709
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Woodward, Richard P. (NASA Lewis Research Center Cleveland, OH, United States)
Loeffler, Irvin J. (NASA Lewis Research Center Cleveland, OH, United States)
Dittmar, James H. (NASA Lewis Research Center Cleveland, OH, United States)