NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Acoustic and turbulence measurements of a tone-excited jet with and without flight simulationAcoustic as well as turbulence measurements were made of tone-excited jets to obtain an understanding of the broadband noise augmentation mechanism. Results for both heated and unheated jets with and without flight simulation are presented for a range of excitation frequencies and levels, as well as for the zero order and first order spinning modes. It is argued that although the phase-locked large-scale turbulence structure is at the root of the noise amplification process, the actual noise generation mechanism lies in the small-scale turbulence. Results show that (1) the phase velocity of the excited large scale instability waves is subsonic relative to the ambient fluid and (2) broadband jet noise is almost uniform at all frequencies. Moreover, when the large-scale and small-scale structures are plotted against forward velocity (for a given upstream excitation level of 141 dB), the change in large-scale turbulence is negligible with forward velocity, whereas the small-scale turbulence decreases for both excited and unexcited jets. Also, the corresponding difference in far-field noise does not appear to change significantly, indicating that the changes in small-scale turbulence are responsible for jet noise amplification.
Document ID
19810064236
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ahuja, K. K.
(Lockheed-Georgia Co. Marietta, GA, United States)
Lepicovsky, J.
(Lockheed-Georgia Co. Marietta, GA, United States)
Burrin, R. H.
(Lockheed-Georgia Co. Marietta, GA, United States)
Date Acquired
August 11, 2013
Publication Date
October 1, 1981
Subject Category
Acoustics
Report/Patent Number
AIAA PAPER 81-2007
Report Number: AIAA PAPER 81-2007
Meeting Information
Meeting: Aeroacoustics Conference
Location: Palo Alto, CA
Start Date: October 5, 1981
End Date: October 7, 1981
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
81A48640
Funding Number(s)
CONTRACT_GRANT: NAS3-21987
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available