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Effect of Pulsed Blowing on Farfield NoiseThis portion of the report documents the results of an experimental program, which focused on pulsed blowing from the trailing edge of a CCW. The main objective of this study was to assess whether pulsed blowing resulted in more, less, or the same amount of radiated noise to the farfield. Results show that a reduction in far-field noise of up to 5 dB is measured when pulse flow is compared to steady flow for an equivalent lift configuration. This reduction is in the spectral region associated with the trailing edge jet noise. This result is due to the unique advantage that pulsed flow has over steady flow. For a range of frequencies, more lift is experienced with the same mass flow as the steady case. Thus, for an equivalent lift and slot height, the pulsed system can operate at lower jet velocities, and hence lower jet noise. At low frequencies (below 1 kHz), the pulsed flow configuration generated more noise in the farfield. This is most likely due to the pulsing mechanism itself. Since the high pressure air feeding the pulsing mechanism was first passed through a high performance muffler, it is likely that this increase in not due to upstream valve noise. Most likely, the impulsive component of the air that periodically fills the plenum causes a broadband source that reaches the farfield. Although the benefit of a pulse trailing edge jet is evident from a mass flow usage and jet noise perspective, attention should be paid towards the design of a viable pulsing system. Future research program in this area should concentrate on the development of a "quiet" pulsing device.
Document ID
20030065819
Acquisition Source
Langley Research Center
Document Type
Other
Authors
Gaeta, R. J.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Ahuja, K. K.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Hellman, B.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Combier, R.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Date Acquired
August 21, 2013
Publication Date
May 31, 2003
Publication Information
Publication: Application of Circulation Control Technology to Airframe Noise Reduction
Subject Category
Aerodynamics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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