NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Controlled excitation of a cold turbulent swirling free jetExperimental results from acoustic excitation of a cold free turbulent jet with and without swirl are presented. A flow with a swirl number of 0.35 (i.e., moderate swirl) is excited internally by plane acoustic waves at a constant sound pressure level and at various frequencies. It is observed that the cold swirling jet is excitable by plane waves, and that the instability waves grow about 50 percent less in peak rms amplitude, and saturate further upstream compared to corresponding waves in a jet without swirl having the same axial mass flux. The preferred Strouhal number based on the mass-averaged axial velocity and nozzle exit diameter for both swirling and nonswirling flows is 0.4. So far no change in the mean velocity components of the swirling jet is observed as a result of excitation.
Document ID
19880054341
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Taghavi, R.
(Kansas University Center for Research, Inc., Lawrence, United States)
Rice, E. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Farokhi, S.
(Kansas, University Lawrence, United States)
Date Acquired
August 13, 2013
Publication Date
April 1, 1988
Publication Information
Publication: ASME, Transactions, Journal of Vibration, Acoustics, Stress, and Reliability in Design
Volume: 110
ISSN: 0739-3717
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
ASME PAPER 87-WA/NCA-18
Accession Number
88A41568
Funding Number(s)
CONTRACT_GRANT: NCC3-56
Distribution Limits
Public
Copyright
Other

Available Downloads

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