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Instability modes excited by natural screech tones in a supersonic rectangular jetThe evolution of hydrodynamic instability modes self-excited by harmonically related natural screech tones was experimentally investigated. A convergent rectangular nozzle with an aspect ratio of 9.63 was used to produce a supersonic shock containing jet. Measurements in the flow-field were made using standard hot-film probes positioned only in the subsonic (outer) portions of the flow. The hydrodynamic instability mode observed in the shear layer at the screech frequency was observed to be antisymmetric (sinuous) about the smaller dimension of the jet, whereas its harmonic was observed to be symmetric (varicose). In addition, the near-field noise measurements indicated that the radiated screech tone noise was out of phase on either side of the small jet dimension whereas its harmonic was in phase over the same region. To our knowledge such an observation on the nature of the harmonic has thus far gone unreported and therefore is the focus of the present work. The hydrodynamic instability modes occurring at the screech frequency and its harmonic satisfied the conditions for resonance. Detailed measurements of the coherent wave evolution in the streamwise and spanwise directions indicated that strong spanwise variations were present beyond x/h = 8. Details of the screech noise radiated by the coherent instability modes are also presented in this paper.
Document ID
19940017801
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Raman, Ganesh
(Sverdrup Technology, Inc. Brook Park, OH., United States)
Rice, Edward J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1993
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.15:106409
AIAA PAPER 93-4321
NASA-TM-106409
E-8246
Report Number: NAS 1.15:106409
Report Number: AIAA PAPER 93-4321
Report Number: NASA-TM-106409
Report Number: E-8246
Meeting Information
Meeting: AIAA Aeroacoustics Conference
Location: Long Beach, CA
Country: United States
Start Date: October 25, 1993
End Date: October 27, 1993
Sponsors: AIAA
Accession Number
94N22274
Funding Number(s)
PROJECT: RTOP 505-62-52
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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