Jet Noise Scaling in Dual Stream NozzlesPower spectral laws in dual stream jets are studied by considering such flows a superposition of appropriate single-stream coaxial jets. Noise generation in each mixing region is modeled using spectral power laws developed earlier for single stream jets as a function of jet temperature and observer angle. Similarity arguments indicate that jet noise in dual stream nozzles may be considered as a composite of four single stream jets representing primary/secondary, secondary/ambient, transition, and fully mixed zones. Frequency filter are designed to highlight spectral contribution from each jet. Predictions are provided at an area ratio of 2.0--bypass ratio from 0.80 to 3.40, and are compared with measurements within a wide range of velocity and temperature ratios. These models suggest that the low frequency noise in unheated jets is dominated by the fully mixed region at all velocity ratios, while the high frequency noise is dominated by the secondary when the velocity ratio is larger than 0.80. Transition and fully mixed jets equally dominate the low frequency noise in heated jets. At velocity ratios less than 0.50, the high frequency noise from primary/bypass becomes a significant contributing factor similar to that in the secondary/ambient jet.
Document ID
20110000527
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Khavaran, Abbas (ASRC Aerospace Corp. Cleveland, OH, United States)
Bridges, James (NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 25, 2013
Publication Date
November 1, 2010
Subject Category
Acoustics
Report/Patent Number
AIAA Paper 2010-3968NASA/TM-2010-216887E-17466Report Number: AIAA Paper 2010-3968Report Number: NASA/TM-2010-216887Report Number: E-17466
Meeting Information
Meeting: 16th Aeroacoustics Conference
Location: Stockholm
Country: Sweden
Start Date: June 7, 2010
End Date: June 9, 2010
Sponsors: American Inst. of Aeronautics and Astronautics, Confederation of European Aerospace Societies