NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Spectra of turbulent static pressure fluctuations in jet mixing layersSpectral similarity laws are derived for the power spectra of turbulent static pressure fluctuations by application of dimensional analysis in the limit of large turbulent Reynolds number. The theory predicts that pressure spectra are generated by three distinct types of interaction in the velocity fields: a fourth order interaction between fluctuating velocities, an interaction between the first order mean shear and the third order velocity fluctuations, and an interaction between the second order mean shear rate and the second order fluctuating velocity. Measurements of one-dimensional power spectra of the turbulent static pressure fluctuations in the driven mixing layer of a subsonic, circular jet are presented, and the spectra are examined for evidence of spectral similarity. Spectral similarity is found for the low wavenumber range when the large scale flow on the centerline of the mixing layer is self-preserving. The data are also consistent with the existence of universal inertial subranges for the spectra of each interaction mode.
Document ID
19770068269
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jones, B. G.
(Illinois Univ. Urbana-Champaign, IL, United States)
Adrian, R. J.
(Illinois Univ. Urbana-Champaign, IL, United States)
Nithianandan, C. K.
(Illinois, University Urbana, Ill., United States)
Planchon, H. P., Jr.
(Westinghouse Electric Corp. Madison, Pa., United States)
Date Acquired
August 9, 2013
Publication Date
October 1, 1977
Subject Category
Acoustics
Report/Patent Number
AIAA PAPER 77-1370
Meeting Information
Meeting: Aeroacoustics Conference
Location: Atlanta, GA
Start Date: October 3, 1977
End Date: October 5, 1977
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
77A51121
Funding Number(s)
CONTRACT_GRANT: NGR-14-005-149
Distribution Limits
Public
Copyright
Other

Available Downloads

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